28 UV Molecular Spectroscopy from Electron Impact for Applications to Planetary Atmospheres and Astrophysics Joseph M. Ajello California Institute of Technology Pasadena, California Rao S. Mangina California Institute of Technology Pasadena, California Robert R. Meier George Mason University Fairfax, Virginia Contents 28.1 28.2 28.3 28.4 Introduction........................................................................................................................... 761 UV Spectroscopy of Molecules in Planetary Atmospheres.................................................. 763 Apparatus and Experimental Methods.................................................................................. 767 Present Status of H2, N2, CO, and SO2.................................................................................. 772 28.4.1 H2–UV....................................................................................................................... 772 28.4.2 H2–VOIR.................................................................................................................... 776 28.4.3 N2–EUV..................................................................................................................... 780 28.4.4 N2–FUV..................................................................................................................... 786 28.4.5 CO.............................................................................................................................. 792 28.4.6 SO2............................................................................................................................. 793 28.5 Conclusions............................................................................................................................ 796 Acknowledgments........................................................................................................................... 797 References....................................................................................................................................... 797 28.1 Introduction In the upper atmospheres and torus regions of the terrestrial and Jovian planets and in the interstellar medium (ISM), an important mechanism for energy transfer and diagnostic spectroscopy is electron collision processes with both neutral and ionic species leading to the emission of electromagnetic radiation. Six of the planets (Earth, Mars, Jupiter, Saturn, Uranus, and Neptune) are known to have internal magnetic fields that lead to particle acceleration and energy deposition into a planetary atmosphere (Bagenal et al., 2007). Mercury also has an intrinsic magnetic 761 762 Charged Particle and Photon Interactions with Matter field with a tenuous atmosphere that is a planetary exosphere. The ubiquitous presence of energetic electron-excited ultraviolet (UV) dayglow and aurora in the solar system (Broadfoot et al., 1979, 1981a,b, 1989; Sandel et al., 1979; Yung et al., 1982; Meier, 1991; Ajello et al., 1998b, 2001, 2005a; Gustin et al., 2002, 2004) has been studied spectroscopically over the last 30 years using observations from interplanetary spacecraft beginning with the Voyager Grand Tour mission and Mars and Venus Mariner missions, and the earth-orbiting satellites beginning with the Orbiting Geophysical Observatories (OGOs) and International Ultraviolet Explorer (IUE). Simultaneously, astronomical observations of H 2 Rydberg band emissions from Herbig-Haro and T-Tauri stellar objects (Raymond et al., 1997; Herczeg et al., 2002, 2004; Bergin et al., 2004) and models of H2 Rydberg band emissions generated in the interior of molecular clouds within the ISM (Gredel et al., 1987, 1989; Liu and Dalgarno, 1996) have been achieved, first with the Copernicus, which was equipped with a UV telescope (Grewing et al., 1978, Snow, 1979), and followed at higher spectral resolution by the Hubble Space Telescope (HST) with its corrected optics (Petersen and Brandt, 1995). The importance of electron impact excitation of molecules was dramatized during the Voyager mission due to findings of rich dayglow and auroral spectra at each of the outer planets with strong magnetospheres and thick H2 atmospheres. For example, the Voyager 1 spacecraft equipped with the ultraviolet spectrometer (UVS), having a detection range of 50–170 nm, arrived at Jupiter in January 1979 and at Saturn in November 1980, and made spectacular discoveries related to the physical processes involving electron acceleration and corotating plasma that control the atmosphere and magnetosphere (Broadfoot et al., 1979, 1981a,b, 1989; Sandel et al., 1979). Voyager discovered that Jupiter’s UV aurora is the second brightest source of UV in the solar system (second to the Sun), with an emission intensity of ∼1013−14 W in the H2 Rydberg bands. Its ultimate power source is the rotational energy of the planet as well as plasma processes in the near corotating middle magnetosphere. The breadth of objects studied with these telescopes is shown in Figure 28.1. In the early 1980s, the initial attempts in modeling the extreme ultraviolet (EUV) auroral spectra obtained by Voyager and other missions were not very successful due to lack of spectroscopic signatures and their reliable cross section data. At this point in time, reliable electron excitation cross sections can only be provided through laboratory measurements, but seldom by theory. Useful earlier reviews can be found for terrestrial auroral spectroscopy in Auroral Physics (Meng et al., 1991), and for emission cross section measurements prior to 1998 for some of the planetary species in Avakyan et al., (1998). The analysis of observations of planetary atmospheres made by HST, Cassini and Far Ultraviolet Spectroscopic Explorer (FUSE), and Earth-orbiting spacecraft Thermosphere Ionosphere Mesosphere Energetics and Dynamics/Global Ultraviolet Imager (TIMED/GUVI), Midcourse Space Experiment (MSX), Defense Meteorological Satellite Program (DMSP), POLAR spacecraft, and Imager for Magnetopause-to-Aurora Global Exploration (IMAGE) require accurate collision FIGURE 28.1 Typical types of objects that are studied by spacecraft equipped with UV observatories are the Earth (Terrestrial Objects), Jupiter (Jovian planets) and the Horse Head nebula (ISM). 763 UV Molecular Spectroscopy from Electron Impact for Astrophysics cross sections. With the advent of the newest generation of high-resolution UV imaging space instruments (e.g., Space Telescope Imaging Spectrograph (STIS) and Faint Object Spectrograph (FOS) with UV spectral resolving power ≈105 onboard HST, the emissions of the outer planets have been examined in much greater detail at better resolution and in different spectral regions than Voyager. 28.2 UV Spectroscopy of Molecules in Planetary Atmospheres To illustrate the key relationships among spectroscopic observations, molecular parameters, and planetary constituents, we present the formalism for the Jovian aurora. Airglow processes are similar except that precipitating particle fluxes are replaced by photoelectron fluxes. A schematic of the Jovian magnetic field interacting with the ionosphere is shown in the upper panel of Figure 28.2 along with a model of the primary + secondary differential electron flux, (electrons/s/cm 2/eV) at various altitudes in the Jovian aurora shown in the lower panel (Ajello et al., 2001, 2005a; Grodent et al., 2001). The auroral UV spectrum produced by the precipitating electrons can be used to estimate Q, the precipitating electron energy flux of the primary particles, and E o, their characteristic energy (Strickland et al., 1995). The modeling of the dynamical magnetosphere–­ionosphere coupling producing the Jovian aurora has been recently described (Bunce and Cowley, 2001; Cowley and Bunce, 2001; Hill, 2001). These authors suggest that the auroral oval indicates the presence of a global-scale Birkeland current system that maps to ∼30Rj. This current system passes planetary angular momentum to the outward moving plasma sheet maintaining the middle magnetosphere in near corotation (Hill, 2001). In the region of upward currents (downward electrons), field-aligned potentials accelerate electrons to Ω J|| J B J|| (a) Differential flux (electron/cm2/s/eV) 1010 (b) 109 108 3000 km 107 Primary 106 105 104 300 km 103 102 0 10 101 102 103 Energy (eV) 104 105 106 FIGURE 28.2 (a) The model of the Jupiter ionosphere–magnetosphere coupling showing the currents for the aurora (Cowley and Bunce, 2001; Hill, 2001), and (b) the electron differential energy distribution of primary + secondary electrons at four altitudes in the Jupiter aurora are distinguished by dashed or solid curves (Ajello et al., 2001, 2005a). The unmarked dotted curve is at 800 km. 764 Charged Particle and Photon Interactions with Matter auroral energies of 10–100 keV (Mauk et al., 2002), which in turn generate UV and visible aurora through electron–molecule collisions that are observed by spacecraft at the Jovian planets. The volume emission rate, Vλ(z) (photons/s/cm3), for a simple molecule H2 spectral line at wavelength, λ, emitted in the aurora of the Jovian planets can be written (Ajello et al., 2001, 2005a) as Vλ ( z ) = g j ( z )ω jm (λ )(1 − η j ) N ( z, T ) (28.1) where g j(z) is the excitation rate (excitations per molecule per second) at altitude z into an upper electronic state j characterized by α, v, and J which are principal quantum number, vibrational level quantum number, and rotational level quantum number, respectively. The index m refers to the quantum numbers β (principle), v (vibrational), and J (rotational) for the lower electronic state. N(z, T) is the atmospheric H2 density at altitude z with a local kinetic temperature T. The quantity ηj is the nonradiative yield of predissociation and pre-ionization for the upper state. ωjm(λ) is the emission branching ratio for the transition j → m at wavelength λ and is given by ω jm (λ ) = A jm Aj (28.2) where Ajm is the Einstein spontaneous transition probability from the upper state j to a lower state m Aj is the total emission transition probability to all lower states The excitation rate, g j(z), is proportional to the sum of the individual excitation rates from a ground state rotational-vibrational level, X(vi, Ji). The individual excitation rates equal to the product of the fraction of molecules in the initial ground state rotational-vibrational level, X(vi, Ji), times the fine structure excitation cross section σij from level i to level j for an electron impact energy, ε, times the electron flux. It is written as g j ( z) = ∫ F(ε, z) ∑ f i Xi (T )σij(ε) d ε , (28.3) where f Xi is the fraction of the H2 molecules in the initial ground vibrational level vi and rotational level Ji (see Ajello et al., 2001, 2005a for notation). The sum extends over the fine structure rotational branches for Σ and Π transitions of H2 in an upper atmosphere. F(ε, z) is the precipitating electron flux distribution function in electrons/sec/cm2/eV at an energy ε and altitude z. The first step in modeling the Jovian aurora requires careful laboratory studies to determine σij (ε) for each rotational line following electron impact excitation of H2 (Liu et al., 1998; GlassMaujean et al., 2009). UV emissions from the outer planets observed by Voyager and IUE were explained with electron transport models of high-energy electron impact (1–100 keV primary electron flux at the top of the atmosphere) of H2 that included all Rydberg states from principal quantum number, n = 2–5 (Yung et al., 1982; Shemanksy and Ajello, 1983; Ajello et al., 1984). Modeling to date (Jonin et al., 2000; Liu et al., 2000, 2002, 2003; Glass-Maujean et al., 2009) now takes into account the rotational-electronic coupling among the n = 2 through 5 states, ungerade B, B′, B″, C, D, D′, D″ (1Σu+, 1Πu) n = 2, 3, 4, 5 → X 1Σg+ and can be used for accurate modeling of the aurora spectra. We show in Figure 28.3a the first model analysis (Yung et al., 1982) (Equations 28.1 through 28.3) of the Jupiter auroral far ultraviolet (FUV) spectrum from IUE. A comparison of this spectrum obtained at 0.1 nm resolution with a model provided convincing proof that most of the emission features come from H2 (Yung et al., 1982). Comparison of a Saturnian auroral spectrum obtained by Voyager in the EUV at 3.3 nm resolution with an auroral model is shown in Figure 28.3b that all of the features could be identified with molecular hydrogen as well (Shemansky and Ajello, 1983). Gustin et al. (2009) has recently analyzed the Cassin ultraviolet imaging spectrograph (UVIS) UV Molecular Spectroscopy from Electron Impact for Astrophysics 765 1 keV IUE data 10 keV 100 keV Aurora 1 keV IUE 10 keV 100 keV 1150 1200 1250 1300 1350 1400 1450 1500 1550 1600 1650 (a) Wavelength (Å) V1 Saturn aurora darkside n.pole Relative intensity Observed data Model e + H2 (all bands) & e+H Model e + H2 (B, C) & e+H H+e Lβ 600 (b) 800 1000 1200 1400 1600 Wavelength (Å) FIGURE 28.3 (a) IUE observation of Jupiter with three auroral models (1, 10, 100 keV primary electrons) in the FUV (Yung et al., 1982). (b) Shown in dash are the Voyager 1 and 2 observation of prominent UV radiation from the atmosphere of Saturn corresponding to auroral emission, which is concentrated in the polar regions, and is excited by high-energy particle precipitation along the magnetic field lines (Shemansky and Ajello, 1983). The strong disk and auroral feature at 1216 Å, which runs off scale, is the hydrogen Ly α line. The H2 band emission between 900 and 1130 Å is the characteristic of the auroral region. We indicate two models of the observations: B and C-states (n = 2 only) and all Rydberg states (n = 2–4). auroral spectrum of Saturn at much higher resolution of 0.4 nm FWHM. The IUE analysis provided the magnitude of both Eo and Q. The characteristic energy for the primary electron flux was estimated to be ∼10 keV. A typical characteristic energy ranging from 5 to 100 keV was found by the UVS in the Galileo orbiter mission to Jupiter (Ajello et al., 1998b, 2001, 2005a) and subsequently by Cassini and HST analyses (Dols et al., 2000; Gustin et al., 2002, 2004; Grodent et al., 2003a,b; Ajello et al., 2005a). The globally averaged electron energy flux precipitating into the Jupiter atmosphere was 0.5–2 erg/cm2/s at the time of the IUE observation (Yung et al., 1982). 766 Charged Particle and Photon Interactions with Matter Jupiter STIS image in Cassini Campaign January 13, 2001 Aurora oval STIS aperture (a) 250 HST oval aurora data Regression model EF, GK,.. Cascade B-direct Atomic O lines 225 200 Signal (kR/Å) 175 150 125 100 75 50 25 (b) 0 1290 1300 1310 1320 1330 Wavelength (Å) 1340 1350 FIGURE 28.4 (a) A Jupiter STIS image taken at 16:50 UT on January 13, 2001, showing the three auroral zones of polar cap, auroral oval and limb with the 52 × 0.5 arcs2 slit projected on the image (Ajello et al., 2005a). (b) The HST STIS G140M medium-resolution grating relative photon intensity short wavelength spectrum (1295–1345 Å) for the north aurora of January 13, 2001 fitted in linear regression. The linear regression analysis with independent vectors of (1) a direct excitation optically thin spectrum of the Rydberg bands of H2 by a monoenergetic electron distribution at 100 eV, (2) a cascade excitation optically thin spectrum of the Rydberg bands of H2 by a monoenergetic electron distribution at 100 eV, and (3) an atomic oxygen multiplet at 1304 Å. The regression model to the observational data is based upon a linear regression analysis with these three independent vectors and transmission through a slab of CH4. We were able to estimate the total contributions from direct excitation and cascading (Ajello et al., 2005a). The atomic O 130.4 nm emission is an artifact of the Earth’s dayglow superimposed on the Jupiter observation. The STIS performed medium- and high-resolution spectral image observations (FWHM = 10 −2 to 10 −3 nm) of Jupiter in the FUV between 115 and 170 nm, revealing the rotational structure of the principal thermospheric gas, H2, in the aurora oval, in the polar cap, and in the Io flux tube. A STIS medium-resolution spectrum and H2 model are shown in Figure 28.4 (Ajello et al., 2005a). The medium-resolution (0.09 nm FWHM, G140 M grating) FUV observations 129.5–134.5 nm by STIS on January 13, 2001 were analyzed using a recently developed high-spectral-resolution model for UV Molecular Spectroscopy from Electron Impact for Astrophysics 767 the electron-excited H2 rotational lines that considered the Lyman Band spectrum (B 1Σu+ → X 1Σg+) to be composed of an allowed direct excitation component (X 1Σg+ → B 1Σu+) and an optically forbid− − den component (X 1Σg+ → EF, GK, H H,… 1Σg+ followed by the cascade transition EF, GK, H H,… 1Σ + → B 1Σ +). The medium-resolution spectral regions for the Jupiter aurora were carefully chosen g u to emphasize the cascade component (Ajello et al., 2005a). 28.3 Apparatus and Experimental Methods In response to the need for accurate collision cross sections to model spectroscopic observations of the terrestrial and Jovian planetary systems, the Emission Spectroscopy Laboratory (ESL) at Jet Propulsion Laboratory (JPL) has established five unique instruments for routinely measuring the absolute emission cross sections of stable and radical gases from the broad spectral region of the UV to the Visible-Optical-Infrared (VOIR) (40–1100 nm). Three of the five instruments are shown in Figure 28.5 and are identified as follows: (1) atomic O (Johnson et al., 2003a,b, 2005), (2) 3 m high resolution (Liu et al., 1995), and (3) atomic H (James et al., 1998a) apparatuses. Not shown in the figure are the VOIR (Aguilar et al., 2008; Ajello et al., 2008; Mangina et al., 2010) and the large chamber for studying the long-lived metastable emissions (Kanik et al., 2003). The 3 m optical spectrometer system is capable of high spectral resolution with a resolving power of λ/Δλ = 50,000 and is equipped with a Codacon 1340 × 400 array detector for studying the rotational structure and kinetic energy (line profiles) of excited fragments (Ajello and Ciocca, 1996a). Each UV spectrometer has dual exit ports and dual grating holders to allow scanning over two wavelength ranges, e.g., the extreme ultraviolet (EUV from 40 to 120 nm), far ultraviolet (FUV from 110 to 310 nm), or visible-optical-near IR (VOIR from 300 to 1100 nm), without breaking the vacuum. Using this instrumentation, ESL has carried out measurements consisting of a calibrated primary data set of optically thin UV and VOIR fluorescence spectra (50–1100 nm) at spectral resolutions between 0.002 and 1 nm and absolute excitation cross sections at electron impact energies 0–2 keV for several stable gases such as H2 (Ajello et al., 1995b, 1996b; James et al., 1998b; Liu et al., 1998, 2000, 2002, 2003; Dziczek et al., 2000; Jonin et al., 2000; Aguilar et al., 2008; Glass-Maujean et al., 2009); HD (Ajello et al., 2005b); D2 (Ciocca et al., 1997a; Abgrall et al., 1999); He (Shemansky et al., 1985); Ar (Ajello et al., 1990); Ne (Kanik et al., 1996); CO (Ciocca et al., 1997b; Zetner et al., 1998; Beegle et al., 1999); CO2 (Kanik et al., 1993); H2O (Makarov et al., 2004), O2 (Noren et al., 2001b; Kanik et al., 2003; Terrell et al., 2004); N2 (Ajello et al., 1998a; Liu et al., 2008, Mangina et al., 2010; Young et al., 2010), SO2 (Ajello et al., 2002a, 2008; Vatti Palle et al., 2004), NO (Ajello et al., 1989a), NO2 (Young et al., 2009), N2O (Malone et al., 2008), and for the radical atomic gases H (James et al., 1997, 1998a) and O (Noren et al., 2001a; Johnson et al., 2003a,b, 2005a). A large number of analyses of data from the wide variety of satellite missions listed above have used the ESL measured cross sections and line profiles (Hord et al., 1992; Ciocca et al., 1997a,b; Prange et al., 1997; Feldman et al., 2001; Gustin et al., 2002; 2004; Esposito et al., 2004). Likewise, the mission planning and instrument calibration phases of the UV instruments on board Cassini and the Pluto New Horizons (Stern et al., 2008) interplanetary spacecraft depended on cross sections, spectra, and spectral line profiles established by the ESL (Ajello et al., 1995a,b). The emission cross sections of the majority of neutral and single-ionized planetary gases have been reviewed by Avakyan et al. (1998) and Majeed and Strickland (1997), and for molecular hydrogen and its isotopes by Tawara et al. (1990). For atomic oxygen, one of the most important planetary gases, and oxygen-bearing molecule’s reviews of cross sections have been given recently by Johnson et al. (2005) and McConkey et al. (2008). The experimental technique developed at JPL for the measurements of electron-impact-induced UV emission cross sections and spectra of stable atoms and molecules has been described in Ajello et al. (1989b, 2002a,b) and references therein, and is shown schematically in Figure 28.6. In brief, UV emission spectra are generated from collision of a collimated beam of energetic electrons with 768 Charged Particle and Photon Interactions with Matter The atomic O experiment Cem Discharge O-Jet XYZ Manipulator O2 N Microwave discharge Pmt e-Beam hν e-Gun UV/VIS Spectrometer To turbos Helmholtz coils HV Spark (a) High resolution 3m UV spectrometer The atomic H experiment Thermal blanket frame Codecon Cem or pmt Gas beam Back focussing mirror XYZ Manipulator hν UV Spectrometer E-Beam Collision chamber H Electrostatic e-GUN UV Light source RF Discharge H2 hνLβ Polarization hν Lα Cross spectrum UV Spectrometer Turbo pump (b) (c) FIGURE 28.5 The JPL instrumentation consisting of: (a) an atomic O radical source with a low-resolution spectrometer, λ/Δλ = 1000 (Johnson et al., 2005); (b) a high-resolution 3 m imaging spectrograph with Codacon MCP detectors similar to the detector flown on Cassini UVIS, λ/Δλ = 50,000 (Liu et al., 1995); and (c) the atomic H radical source with low-resolution spectrometer, λ/Δλ = 1000 (James et al., 1997). a beam of target gas (produced by a capillary array) in a crossed-beams geometry at a background pressure that ensures optically thin, single-scattering conditions. The interaction volume of the crossed beams is approximately 2 mm3. Emitted photons corresponding to the radiative decay of collisionally excited states of the target species are detected by the UV spectrometer with its optic axis at 54.74° (magic angle) or 90° to the plane containing the crossed electron- and target molecular beams. UV Molecular Spectroscopy from Electron Impact for Astrophysics 769 Electron collision processes study of neutral species Apparatus VUV (40–500 nm) Spectrometer (λ/Δλ = 50,000) Collison chamber e (0–2 keV) hν hν M (H, H2, O, …) Pulse (a) Spectrum (40–500 nm) e+M M* M*+ eS M+ hνspectrum Excitation function (0–2 keV) e+M M* M+ hνexcitation function λ selected σ (cm2) Energy selected l (b) M*+ eS λ (nm) (c) Energy (eV) FIGURE 28.6 (a) A schematic of the crossed electron beam-molecular-beam apparatus for (b) measuring electron-impact-induced fluorescence spectra and (c) emission cross sections as a function of excitation energy measurement by continually scanning electron energy, e.g., from 0 to 2 keV. In an electron-impact-induced emission experiment, a molecule in a ground electronic X-state is excited to an electronic state α. A model of the irradiance from the interaction region for the transition │α, v, J〉 → │X, vf, Jf〉 from a target molecule, such as H2 or CO, is based on the calculated transition probabilities (e.g., for H2 Lyman and Werner bands use Abgrall et al. (1993a,b,c, 1997, 1999, 2000) and the rotational line positions of Roncin and Launay (1994)). For the CO Fourth Positive system, we use the transition probabilities and molecular constants given in Morton and Noreau (1994). The model for electron-excited H2 molecules has been presented in previous papers (Liu et al., 1995, 1998, 2000, 2003; Jonin et al., 2000). We will briefly describe it here. The populations of the ground-state rotational levels are controlled by the gas temperature and nuclear spin of the molecule. The ground-state molecules in vibrational and rotational thermal equilibrium are excited into the various rovibronic states according to the excitation rate g′ (α, v, J, Ee). The photoemission intensity into the various branches from rovibronic state │α, v, J〉 is partitioned according to the emission branching ratio, predissociation yield, and pre-ionization yield. The photoemission volume intensity, V′ (photons/s/cm3), at any given point (x, y, z) in the interaction region defined by the intersection of electron beam of energy Ee and molecular beam, in the laboratory, including selfabsorption and predissociation, is given by V ′( X , α, vf , v, J f , J ) = A( X , α, vf , v, J f , J ) ⋅ g′(α, v, J , Ee ) ⋅ (1 − ηP (α, v, J )) ⋅ Tr( X , α, v, J , T ) (28.4) A( X , α, v, J ) 770 Charged Particle and Photon Interactions with Matter A( X , α, v, J ) = ∑ A( X, α, v , v, J , J ) f (28.5) f vf , J f where A(X, α, vf, v, Jf, J) is the Einstein A-coefficient for spontaneous transition from the excited state │α, v, J〉 back to │X, vf, Jf〉 of the X 1Σg+ ground state A(X, α, v, J) is the total emission probability (including transitions to lower singlet-gerade states and to the continuum levels of the X 1Σg+ state) ηP(α, v, J) is the predissociation + pre-ionization yield Tr(X, α, v, J, T) is the transmission function for self-absorption by resonance lines The volumetric excitation rate (excitations/s/cm3) at that point (x, y, z) is given by g′(α, v, J , Ee ) = Fe ∑ N σ (E ) i (28.6) e ij i We use the index i to represent the initial electronic state |X, vi, Ji〉, the index j to represent the excited electronic state |α, v, J〉, Ni = No × fxi and the excitation cross section, σij = σ(vi, v, Ji, J). The volumetric excitation rate g′(α, v, J, Ee) is proportional to the population density Ni of the molecule in the initial vibrational–rotational level vi, Ji, and the monoenergetic electron-impact flux Fe due to the electron beam current (Glass-Maujean et al., 2009). Equations 28.4 and 28.6 can be used to define a P, Q, or R branch rotational line emission cross section (without cascade) between two electronic states X and α: σ em (α, X , v, vf , J , J f ) = A( X , α, vf , v, J f , J ) (1 − ηJ ) σ ex ( X , α, vi , v, J i , J , Ee ) A( X , α, v, J ) ν ,J ∑ i i (28.7) The total thermally averaged excitation cross section for an electronic band system is defined by Glass-Maujean et al. (2009) as σ ex = (∑ i, j Ni σij ( Ee ) N0 ) (28.8) and the corresponding thermally averaged emission cross section is given by σ em = ∑ i, j Niσij ( Ee )(1 − η j ) N0 (28.9) The individual rovibronic excitation cross sections σij(Ee) can be calculated from a known transition probability and a measured excitation function for H2 (Liu et al., 1998). For negligible self-absorption, the total band system volumetric photoemission intensity in Equation 28.4 is proportional to the total emission cross section, σem, and the neutral gas density, N0. The σem is related to σex as indicated by comparing Equations 28.8 and 28.9. The ratio σem divided by σex gives the thermally averaged emission yields for each of the ungerade Rydberg states in Table 28.1 (Glass-Maujean et al., 2009). 771 UV Molecular Spectroscopy from Electron Impact for Astrophysics TABLE 28.1 Electronic-Band Cross Sections and Emission Yields of H2 Singlet-Ungerade Statesa State B 1Σu+ C 1Πu B′ 1Σu+ D 1Πu+ D 1Πu− B″ B 1Σu+ D′ 1Πu+ D′ 1Πu− D″ 1Πu 5pσ 1Σu+ 6pσ 1Σu+ 6pπ 1Πu 7pπ 1Σu+ Present σex Previous σex Present σem Previous σem Present Emission Yield (%) Previous Emission Yield (%) 264b 244b 36b 25 21 11 9.3 7.3 3.2 — — — — 262c 241c 38d,e 24d 18d >4d 7.1d 263 249b 21 11 21 2.2 1.6 5.7 0.9 1.1 0.6 0.9 0.6 262c 241c 21d 11d 18d 1.6d 1.0d 5.3d 0.6 — — — — 99b 98b 53 43 100 20 18 78 28 — — — — 100 100 56 46 100 <40 14 ≥5.3d >0.6 — — — — ≤100 — — — — — Source: Glass-Maujean, M. et al., Astrophys. J. Suppl., 180, 38, 2009. With permission. E = 100 eV and T = 300 K. Unit is 10−19 cm2. σex and σem denote excitation and emission cross sections, respectively. Certain numbers may not add up due to roundings. See Section 28.5.3 (Glass-Maujean et al., 2009) for estimated errors in cross sections. b Excitation cross sections include the excitation into the H(1s) + H(2l) continuum, which is estimated from the calculation of Glass-Maujean (1986). Emission cross sections exclude emission from the H(1s)+H(2l) continuum levels, but include continuum emission from the excited discrete levels into the continuum levels of the X 1Σg+ state. Transitions to the X 1Σg+ continuum contribute 27.5% and 1.5%, respectively, to total emission cross sections of B 1Σ + − X 1Σ + and C 1Π − X 1Σ + (Abgrall et al. 1997). Note correction to B′ 1Σ + present σ , u g u g u ex as suggested by Liu (private communication, 2010). c From Liu et al. (1998). d From Jonin et al. (2000). e Include excitations into the continuum levels of the B 1Σ + state. u a The UV wavelength calibration methodology developed at JPL has been used by several spacecraft missions (Hord et al., 1992; Esposito et al., 2004). This technique coupled with a relative flow or swarm gas calibration developed at JPL (Ajello et al., 1989b) allows the determination of absolute emission cross sections σem from any of the ESL optical instrument systems. Recent work by the ESL has established benchmark standards for absolute emission cross sections by electron-impact fluorescence measurements at 100 eV for reference gas H 2 (121.6 nm) σem = 7.03 ± 0.47 × 10 −18 cm 2 (McConkey et al., 2008) and reference gas N2 (120 nm) σem = 3.7 ± 0.5 × 10 −18 cm 2 (Malone et al., 2008). The absolute cross section for the emission of a particular spectral line λ induced by electron impact on a target species M in a swarm gas experiment at 90° to the electron beam can be measured at low pressure as (Johnson et al., 2003a,b) σ( M ) λ = KSλ (1 − (pλ /3)) ξbλ PI e (28.10) 772 Charged Particle and Photon Interactions with Matter where Sλ is the photon signal K is a constant related to the geometry of the detector bλ is the sensitivity of the detector ξ is the instrumental polarization sensitivity of the system pλ is the polarization of the emitted radiation P is the gas pressure Ie is the electron beam current The trapping of resonance radiation can reduce the emission rate significantly at high gas pressure. To avoid this complication, the gas pressure range is maintained at a sufficiently low level. K is determined from an intensity measurement of the known N2 120 nm or H2 121.6 nm emissions, since the instrumental factors are common to both target species (standard and target gas M). At 100 eV, the atomic multiplets from dissociative excitation are unpolarized since many repulsive states contribute to the emissions. 28.4 Present Status OF H2, N2, CO, and SO2 28.4.1 H2–UV Hydrogen is by far the most abundant element in the universe, playing a pivotal role in many physical and chemical processes. For example, in diffuse molecular clouds of the ISM and stellar atmospheres, hydrogen chemistry permeates astronomical changes and provides the markers of stellar evolution (Dalgarno, 1993, 1995). Over the past two decades, the observations of the ISM have shown that H2 is an active component of star formation. The changes that a star undergoes during the formation and dying process are truly dramatic. These result in the most important interactions between a star and its environment. Indeed, it is in this area of research that some of the most challenging astrophysical problems remain unanswered. UV and near-IR emissions from H2 are among the principal ways the interstellar gas cools following gravitational collapse during the star formation (Lepp and Dalgarno, 1996; Lepp et al., 2002). During the last 10 years, the observations of the distribution of H2 gas throughout the galaxy by FUSE have contributed to our understanding of stellar evolution (Moos et al., 2000). Hence, H2 has a unique and extraordinary position in astronomy by virtue of its UV spectroscopic signature of diverse energetic environments. Molecular hydrogen is the simplest molecule from a structural point of view, but its band spectra are quite complex and extend from UV to near-IR wavelengths due to the relatively large values of rotational constants for all the electronic states. An accurate model of the H2 spectrum has been a fundamental building block for understanding the chemistry of the solar system and ISM. Until recently, a 50%–200% uncertainty existed for some of the excitation cross sections and transition probabilities of the singlet-gerade (even) states of H2 and HD, i.e., the states that provide VOIR cascade excitation to the Lyman and Werner bands (Ajello et al., 2005b; Aguilar et al., 2008). The recent study of H2 emission cross sections (Aguilar et al., 2008) is the first of the VOIR wavelength range (300–1100 nm) in 50 years, since the pioneering work of Dieke and coworkers (Dieke, 1958; Dieke and Cunningham, 1965; Crosswhite, 1972) who demonstrated the existence of over 100,000 rotational lines and transitions in this wavelength region involving 15 electronic states of H2 (Crosswhite, 1972). The complete single-scattering VOIR spectra of the H2 and HD gerade– ungerade band systems had never been studied in the laboratory, nor have the oscillator strengths been accurately calculated until recently. The theoretical oscillator strength study by the Meudon Observatory (Aguilar et al., 2008 and references there in) involves detailed calculations of emission transition probabilities and line positions of individual rotational lines of the nine coupled EF, GK, HH, K, P 1Σg+ states and I, R 1Πg and J, S 1Δg+ states. All of these coupled states contribute heavily to the UV spectrum through cascading. Comparing the laboratory spectra to model calculations based UV Molecular Spectroscopy from Electron Impact for Astrophysics 773 on the theoretical oscillator strengths, many irregularities (intensity and wavelength positions) in the VOIR were explained (Aguilar et al., 2008), although many remain unaccounted for and are being reevaluated. The ESL has provided the same molecular parameters for the singlet-ungerade (odd) states of H2 and HD (and even of D2) to an accuracy of 10% (i.e., states that lead to the direct excitation of the Lyman and Werner bands) (Liu et al., 1995; 1998; 2000; 2002; 2003; Abgrall et al., 1999; Ajello et al., 2005b; Glass-Maujean et al., 2009). These will aid in the studies of the ISM and planetary atmospheres, where both types of electron-excited transitions take place. Very accurate synthetic spectral models of H2 for UV astronomy have been developed recently (Dols et al., 2000; Jonin et al., 2000; Liu et al., 2003; Gustin et al., 2004; Glass-Maujean et al., 2009). These models properly account for cascade, predissociation, and resonance effects by utilizing high-resolution measurements of spectra and cross sections (Glass-Maujean et al. 2009). We now understand that the complexity of the H2 band system arises from intense configuration interaction, predissociation, and autoionization that are present in the 11–16 eV electronic energy region of the Rydberg and valence (RV) states. A simplified adiabatic energy level diagram of H2 exhibiting the strongest allowed excitation process producing the B → X (Lyman bands) and the strongest optically forbidden process producing the EF → B (Lyman band cascade) is shown in Figure 28.7. 15 14 13 Potential energy (eV) 12 11 H2 τ = 21 ns τ = 99 ns τ = 200 ns H 1Σ+g 0 G, K 1Σ+g hν(MUV) E, F 1Σ+ 5 2 0 0 g 5 hν(Visible-IR) τ = 2 ns 0 5 τ = 1.1 μs B 1Σu+ hν(Lyman bands) 4 10 3 2 5 1 0 x 1Σ+g 0 0.8 1.6 2.4 3.2 Internuclear distance (Å) FIGURE 28.7 A partial energy level diagram for H2 showing the energy regions for the VOIR (geradeungerade) singlet transitions and the UV (ungerade-gerade) transitions (Aguilar et al., 2008). The lowest-lying ungerade–gerade transition is B 1Σu+ → X 1Σg+ (direct excitation of the Lyman bands) and the lowest-lying gerade–ungerade transition is E, F 1Σg+ → B 1Πu → X 1Σg+ (cascade excitation of the Lyman bands). The approximate lifetimes for some of the direct (dipole-allowed) and cascade (optically forbidden) vibronic states are listed. 774 Charged Particle and Photon Interactions with Matter D 1Πu 1sσnpπ n = 3 Intensity (arb. units) X4 B΄1Σu 1sσnpσ n = 3 X4 B(Lyman) 1Σu 1sσnpσ n = 2 C(Werner) 1Πu 1sσnpπ n = 2 800 1000 1400 1200 Wavelength (Å) 1600 1800 FIGURE 28.8 Model line spectrum of the B 1Σg+ → X 1Σg+, C 1Πu → X 1Σg+, B′ 1 ∑ +u → X 1∑ g+ , and D 1Πu → X 1Σg+ band systems of H2 at 300 K and 100 eV without self-absorption. The model is based on the line positions and transition probabilities of Abgrall et al. (1993a,b,c, 1994, 1997) and the electron emission cross sections of Liu et al. (1998). Shemansky and Ajello (1983) identified, for the first time, the presence of the two most important UV emissions in the observations by the Voyager I, II spacecraft for application to the outer planets. These are the Rydberg series of H2, namely, 1Σu+ 1sσnpσ (B, B′, B″, n = 2, 3, 4) → X 1Σg+ and 1Π 1sσnpπ (C, D, D′, D″, n = 2, 3, 4, 5) → X 1Σ + through n = 5, along with optically forbidden exciu g tation of X 1Σg+ → EF 1Σg+ followed by dipole-allowed cascade of EF 1Σg+ → B 1Σu+, which were found to be the indicators of electron energy and were the source of the principal (overlapping) spectral contributions to the Voyager UV spectrum (Shemansky and Ajello, 1983; Ajello et al., 1984; Jonin et al., 2000). Prior to this work, the Lyman and Werner band systems (n = 2) were thought to be the only bands involved in the Voyager analysis (Broadfoot et al., 1979, 1981a,b), as shown in Figure 28.3a. In Figure 28.8, we show (to scale) a composite of the first four (n = 2, 3) of the 15 singlet-state band systems contributing directly to the H2 UV spectrum (Liu et al., 1995; Ajello et al., 2001). Over the last 20 years, a study has been carried out of the remaining singlet-ungerade states in the high-resolution EUV emission spectra of molecular hydrogen excited by electron impact at 100 eV under optically thin, single-scattering experimental conditions (Jonin et al., 2000; Liu et al., 2000; Glass-Maujean et al., 2009). A portion (94.5–96 nm) of the high resolution spectrum (FWHM = 0.0085 nm) spanning the wavelength range of 80–115 nm is shown in Figure 28.9. The total emission cross sections for D 1Πu, D′ 1Πu, D″ 1Πu, B′ 1Σu+, B″ 1Σu+ states for the n = 3 and four transitions to the ground state were obtained at 100 eV by measuring the emission cross section of each rotational line. The Lyman and Werner bands have the largest emission cross sections at 100 eV with values of 2.64 × 10 −17 cm2 and 2.44 × 10 −17 cm2, respectively (Liu et al., 1998; Jonin et al., 2000; Glass-Maujean et al., 2009). Glass-Maujean et al. (2009) now give the 100 eV electronic Rydberg band system emission and excitation cross sections through n = 7. We list these cross sections in Table 28.1. 775 UV Molecular Spectroscopy from Electron Impact for Astrophysics 1.4 1(3,0)Q C-X 1(0,2)R D-X 4(3,0)R C-X 1(0,2)Q D-X 1(13,0)R B-X 3(5,1)P C-X 3(0,2)Q D-X 2(13,0)R B-X 3(0,2)Q D-X 2(13,0)P B-X 5(3,0)P C-X 1(0,2)R D-X 1(1,2)R B-X 3(18,1)P B-X 948 3(3,0)P C-X 946 3(19,1)P B-X 3(2,3)Q D-X 2(5,1)Q C-X 0.2 3(3,0)Q C-X 1(5,1)R C-X 3(2,3)P D-X 0.4 B, B΄, C, D Experiment ΔλFWHM = 140 mÅ Theory 3(4,4)Q D-X 2(3,0)Q C-X 1(2,3)Q D-X 2(14,0)P B-X atomic line 1s-5p 0.6 0(3,0)R C-X 1(14,0)R B-X 1.0 0.8 e (100 eV) + H2 (300 K) 1(4,4)Q D-X Calibrated intensity (arb. units) 1.2 0.0 950 952 954 Wavelength (Å) 956 958 960 FIGURE 28.9 Over-plot of the observed spectra (FWHM = 140 m Å) and model spectra of H2 for the low pressure regime of background pressure of 1.2 × 10 −5 Torr. The high-pressure spectrum spans the wavelength range from 945 to 960 Å. The model uses the transition probabilities of Abgrall et al. (1993a,b,c, 1994, 1997) with a transmission function for self-absorption at 100 eV electron-impact energy and a gas temperature of 300 K. For J values of 1–4 at laboratory temperatures of ∼300 K, the emission yields of each rovibronic level of the npσ 1Σu+ and npπ 1Πu states are determined by comparing observed and calculated rotational spectra (Glass-Maujean et al., 2009). Since Jovian aurora take place at elevated rotational temperatures of 500–1200 K (Gustin et al., 2004), models of the EUV require predissociation yields to high J-value (∼J = 5–10) (Glass-Maujean et al., 2009). In summary, the mean emission yields of the B 1Σu+, C 1Πu, B′ 1Σu+, D 1Πu+, D 1Πu−, B″ 1Σu+, D′ 1Πu+, D′ 1Πu−, D″ 1Πu states, defined previously, are 99%, 98%, 53%, 43%, 100%, 20%, 18%, 78%, 28%, respectively, at 100 eV and 300 K (GlassMaujean et al., 2009) (see Table 28.1). Using the Q1(1,4) Werner rovibronic line and the P1,2,3(8,14) Lyman rovibronic line, we developed an accurate modified Born model for the excitation cross section (without cascade) of the Lyman and Werner bands for use in the electron transport codes of planetary atmospheres and astrophysics. The model for 0–1.2 keV electron impact energy is shown in Figure 28.10 with the updated Lyman and Werner 100 eV cross sections (Liu et al., 1998; Glass-Maujean et al., 2009). Glass-Maujean et al. (2009) give estimates for excitation functions for the B″ and D′-states. An accurate model of a 100 eV high-resolution laboratory electron-impact-induced fluorescence spectrum, based on the calculated transition probabilities and predissociation yields of Abgrall et al., (1993a,b,c) and Glass-Maujean et al., (2007a,b,c,d, 2008), verifies adiabatic transition probabilities for RV rovibronic states of n = 4–8 and nonadiabatic transition probabilities for n = 2–4. The synthetic spectrum is capable of modeling over 98% of the laboratory e + H2 emission spectrum at room temperature 300 K and 100 eV electron energy. Furthermore, the Lyman and Werner emission cross section energy dependence from Liu et al. (1998) for the B and C states, and the rotational line positions from Roncin and Launay (1994) have allowed us to generate an accurate (∼15% accuracy from 79 to 90 nm and ∼5% from 90 to 175 nm) synthetic high-resolution rotational line spectrum of the singlet-ungerade states in the UV with electron energies of 10–1000 eV. Using the recent work 776 Charged Particle and Photon Interactions with Matter 100 eV 300 250 Werner Lyman σ (10–19 cm2) 200 150 100 50 0 0 100 200 300 400 500 600 700 800 900 1000 1100 1200 Excitation energy (eV) FIGURE 28.10 Total cross section (in 10 −19 cm2) of the Lyman and Werner band systems at 300 K. The cross section of the Lyman band system is represented by dots, while that of the Werner band system is shown by the solid line (Liu et al., 1998; Glass-Maujean et al., 2009). of Glass-Maujean et al. (2007a,b,c,d, 2009) and comparing the synthetic spectra through n = 8 with the ESL high-resolution spectra, it has been possible to accurately model direct excitation to the high-lying, ungerade-singlet Rydberg states. The high-lying states contribute significantly to the EUV spectrum below 90 nm. 28.4.2 H2–VOIR The electron-impact-induced fluorescence spectrum of H2 from 330 to 1000 nm at 20 and 100 eV was reported for the first time (Aguilar et al., 2008) at high resolution (λ/Δλ = 10,000). The spectrum − contains the gerade Rydberg series of singlet states EF 1Σg+, GK 1Σg+, H H 1Σg+, I 1Πg, J 1Δg … → B 1Σu+, 1 3 3 C Π and the Rydberg series of triplet states dominated by the d Πu, k Πu, j 3Δg → a 3Σg+, C 3Πu. These VOIR bands were recently observed by the Cassini Imaging Subsystem (ISS) in the visible/near IR filters viewing the Saturn aurora (Dyudina et al., 2007). STIS or Cosmic Origins Spectrograph (COS) might also be able to observe these directly on the outer planets. A model VOIR spectrum of H2 from 750 to 1000 nm, based on newly calculated transition probabilities and line positions, including rovibrational coupling for the singlet-gerade states, is in excellent agreement with the observed intensities. Figure 28.11 shows the experimental data of high-resolution (0.07 nm FWHM), electron-impact-induced UV-VOIR emission spectra from 330 to 1200 nm at 100 eV. The absolute emission cross section values for excitation to the singlet-gerade states at 100 eV for optically thin, single-scattering condition was measured to be 4.58 ± 1.37 × 10 −18 cm2; for excitation to the triplet states at 20 eV, the cross section was 1.38 ± 0.41 × 10 −19 cm2 (Aguilar et al., 2008). The singlet-gerade emission cross sections are due to cascading into the UV (including the Lyman and Werner band systems), and the triplet-state emission cross sections are due to cascade dissociation of the H2(a 3Σg+ − b 3Σu+) continuum that produces fast hydrogen atoms (Ajello and Shemansky, 1993). In a complementary type of experiment to the VOIR, a newly devised pulsed spectroscopic − technique demonstrated (Dziczek et al., 2000; Liu et al., 2002) that the gerade series (EF, GK, H H, I, J…) make a significant contribution (∼50% at 20 eV) to the UV spectrum of H2, by virtue of their cascade to states that correlate to H(1s) and H(2s,2p) (i.e., the upper states of the Lyman and Werner 777 UV Molecular Spectroscopy from Electron Impact for Astrophysics Hα 0.35 Grating 2 Grating 3 0.30 Theory Cross section (Mb) 0.25 EF-B bands 0.20 0.15 Hβ 0.10 0.05 0.00 –0.05 3000 4000 5000 6000 7000 8000 9000 10000 11000 12000 Wavelength (Å) FIGURE 28.11 High-resolution spectrum with intensity in units of cross section (cm2) for the electron-impactinduced fluorescence spectrum from 3,300 to12,000 Å of H2 at 100 eV in three wavelength regions: (1) grating-2 (3300–7500 Å) in black, grating-3 (7,500–10,000 Å) in long-dash light gray, and theory (10,000–12,000 Å) in short-dash dark gray. The Hα multiplet is off scale (Aguilar et al., 2008). bands, respectively). This large cascade cross section is important because the mean secondary electron energy in planetary thermosphere and in cosmic-ray-induced ionization in molecular cloud lies between 20 and 100 eV (Gredel et al., 1989; Ajello et al., 2002a, 2005b). The intensity of UV resonance transitions excited by electron impact is determined by both the direct and cascade processes. The lifetime (τ) for decay by spontaneous emission from a dipole-allowed transition is typically short (<10 ns, see Figure 28.7). To measure the electron-impact cascade spectrum of the n = 2 H2 Lyman band system (B 1Σu+ − X 1Σg+), we use the longer lifetimes (>30 ns, see Figure 28.7) − for cascade from higher lying states (EF, GK, H H, … 1Σg+). The pulsed gun technique takes advantage of the drastic difference in lifetimes (∼1 ns vs. ∼100 ns) between the ungerade (direct) states and singlet-gerade (cascade) states, respectively. The first laboratory studies and modeling of the UV spectrum of H2 attributed to cascade used a pulsed gun technique to separate cascade and direct excitation effects (Dziczek et al., 2000; Liu et al., 2002). Pulsing the electron gun and gating the photon detector to measure the cascade spectrum after the directly excited population decays also allows a determination of the cascade cross section because the spectral pattern from direct excitation and cascade are different. Direct excitation produces a large population in the B-state centered at v′ = 7, whereas cascade populates the lower vibrational levels most strongly, beginning at v′ = 0. By studying Figure 28.12, we clearly see that there are regions in the FUV spectrum dominated by cascading. The most important two wavelength regions that are exclusively (more than 90%) due to cascade lie near the 133–135 and 139–142 nm. These regions correspond to the rotational lines of the (0,1) and (0,2) vibrational bands of the B−X Lyman bands, the two strongest bands of the v′ = (0, v″) progression. The strongest feature in the cascade spectrum occurs at 161 nm and involves the superposition of rovibronic transitions from v′ = 4, 5, and 6. The medium-resolution spectrum at 14 eV is shown in Figure 28.13b in both the FUV- and middle ultraviolet (MUV) portion of the VOIR extending from 100 to 530 nm, including the Lyman bands and the H2(a 3Σg+ → b 3Σu+) continuum (James et al., 1998b). The first detection of the H2 a-b continuum MUV emission in astronomy (Pryor et al., 1998) was made through comparison to our 778 Charged Particle and Photon Interactions with Matter 20 eV DC spectrum Relative intensity (arb. units) 3.0 20 eV pulse spectrum Model 20 eV spectrum (no cascade) 2.5 2.0 1.5 1.0 0.5 0.0 90 100 110 120 130 140 150 160 170 Wavelength (nm) FIGURE 28.12 The 20 eV steady state (cascade + direct) spectrum and linear regression fit using the 20 eV pulsed-gun cascade spectrum and 20 eV model direct excitation spectrum. H Lα is included in the model as a monochromatic line. The photon gate delay for the pulsed-gun spectrum is 135 ns (Dziczek et al., 2000). H2 MUV spectrum Galileo 400 300 200 100 0 –100 –200 Counts Dark side – Scaled day side Lab 14 eV e– on H2 spectrum H2 (a – b) (First observation in astronomy) 2000 (a) 2500 Wavelength (Å) 3000 Laboratory Relative intensity (arb. units) 1.0 H2 14 eV 0.9 0.8 F-PMT 0.7 a 3Σ+g E-PMT 0.6 b x5 0.5 0.4 x 1Σ+g H2 (a–b) 0.3 hva–b H+H (e–3 eV) 3 + Σu 0.2 0.1 (b) 0.0 100 150 200 250 300 350 Wavelength (nm) 400 450 500 FIGURE 28.13 (a) The first observation in astronomy of the H2 a-b continuum. Jupiter darkside aurora spectrum overplotted with a 14 eV laboratory spectrum (Proyor et al., 1998). (b) The combined FUV spectrum, measured with an EMR F-photomultiplier (CeTe photocathode), and the MUV spectrum, measured with an EMR –E-photomultiplier, of H2 corrected for instrument sensitivity produced by electron impact at 14 eV measured at 1.7 nm FWHM at 300 K and 2 × 10 −4 Torr background gas pressure in the crossed-beams mode (James et al., 1998a,b). 779 UV Molecular Spectroscopy from Electron Impact for Astrophysics laboratory spectrum (James et al., 1998b). We show the comparison of the Galileo observation of the Jupiter dark side aurora with the laboratory spectrum in Figure 28.13a. The set of triplet states above the b 1Σu+ repulsive state leads to continuous emission with high-velocity H-atoms (∼3 eV per atom) formed in the spontaneous dissociation. This process of electron excitation is shown in the inset to Figure 28.13b. The b 3Σu+ state, which is the lowest lying repulsive state (1sσ) (2pσ), can be excited to the continuum by direct excitation from the ground X 1Σg+ state or via cascade from the a 3Σg+ − b 3Σu+ continuum. The a 3Σg+ state produces the strongest triplet-state emission from the process H 2 (a 3Σu+ → b 3Σg+), leading to the famous a-b continuum, for electron energies below 30 eV (Ajello and Shemansky, 1993). The a 3Σu+ state is strongly populated by cascade from the c-, d-, and e-states. The excitation function for the a-b continuum is shown in Figure 28.14. The figure (see inset) also shows a 20 eV spectrum indicating relative importance and wavelength region for strong cascade and a-b continuum in the FUV. The triplet states are the major source of dissociation of the hydrogen molecule by electron impact. Optical excitation functions of the triplet states have also been measured by few experimenters in the VOIR. Dieke (Crosswhite, 1972) has shown the presence of many triplet band systems in his discharge emission experiments with the strongest and most extensive to be the Fulcher-α band system (3pπ d 3Πu → 2sσ a 3Σg+). The emission cross sections of the Fulcher-α diagonal bands (Δv = 0) have been studied by Möhlmann and de Heer (1976). Those processes leading to triplet emissions arise first from singlet–triplet excitation. The excitation occurs by electron exchange, which is characterized by a fast rise and decrease in the emission cross section within a few eV of threshold (see Figure 28.14). Tawara et al. (1990) have reviewed the excitation cross sections of the X → 2sσ a 3Σg+, 2pσ b 3Σu+, 2pπ c 3Πu, and 3pσ e 3Σu+ states by electron-energy-loss experimental techniques. Emission from the e 3Σu+ triplet state e → a transition was observed by Dieke (1958) and Dieke and Cunnigham (1965) as well as by Dieke in a couple of early publications as referenced by Huber and Herzberg (1979) and Crosswhite (1972). The c-state, whose v′ = 0 level lies below the a-state, is forbidden for transitions to the b- and X-state. Thus, there are two Rydberg series terminating in the two bound triplet states, 1.0 1.0 Relative cross section (arb. units) Relative intensity (arb. units) H2 (a – b, 190 nm) Δλ = 10 nm Lα 121.57 nm H2+ e (20 eV) Δλ = 0.5 nm X 1Σ+g B 1Σ+u Lyman bands Direct + cascade a 3Σ+g b 3Σ+u Q = 190 nm 0 110 120 130 140 150 160 170 180 190 200 210 Wavelength (nm) 0 0 50 100 Energy (eV) 150 200 FIGURE 28.14 The H2(a 3Σg+ → b 3Σu+) excitation function from 0 to 200 eV (Ajello and Shemansky, 1993). The inset is a combined FUV and MUV spectrum of H2(a 3Σg+ → b 3Σu+) continuum at 20 eV. The cross-hatched area shows the band pass of the spectrometer for the excitation function measurement. 780 Charged Particle and Photon Interactions with Matter 1600 B-X 1400 Direct + cascade 1200 1000 Cross section (arb. unit) Cross section (arb. unit) 1800 800 1800 1600 1400 1200 1000 800 600 400 200 0 10 600 20 30 40 Energy (eV) 50 60 400 200 Observed 0 Dipole-allowed 0 200 400 600 800 1000 Energy (eV) 1200 1400 1600 1800 FIGURE 28.15 Comparison of the observed H2 B-X dipole-allowed direct + dipole-forbidden cascade excitation function for v = 0 (solid), compared to the v > 7 dipole-allowed excitation function (dotted). The inset shows the threshold behavior of the direct excitation and total cross section. The total cross section demonstrates the existence of resonance excitation and cascading for the low vibrational levels (0–4) near 15 eV (Liu et al., 2003). a and c. Excited triplet states undergoing transitions to either the a- or c-state are thereby forbidden by the g ↔ u rule for transitions to both final states. An additional important topic related to low-energy electron excitation of the RV states of H2 involves resonance excitation, especially of the Lyman bands. We have recently published an analytic model for the n = 2 Lyman band system (B 1Σu+ → X 1Σg+) of H2 (Liu et al., 2003) that is accurate at threshold. We have shown in Figure 28.15 (inset) that for the B 1Σu+ state, the measurement of the UV excitation function of a single rotational line of a low vibrational level (0–4) contains near threshold structure arising from a combination of resonance, dipole-forbidden, and dipole-allowed components. Figure 28.15 shows a measurement of the B 1Σu+ (0,4) P3 high-resolution excitation function. The v′ = 0 excitation function is composed of three processes: (1) direct excitation (see dotted component in Figure 28.15); (2) resonance excitation of H2− autoionizing states (see first peak in inset at ∼13 eV); and (3) a dipole-forbidden excitation from (n = 2) EF, (n = 3) GK, (n = 4) − HH 1Σg+ → B 1Σu+ gerade state cascading. The competition between UV emission production by the band systems of the singlet states and dissociative production of fast H(1s) atoms is a very sensitive function of electron energy in the threshold energy region of 10–50 eV. This allows the mean electron impact energy to be unfolded from astronomical regimes, as was done with Voyager spectral observations of the outer planets. 28.4.3 N2–EUV The strongest dipole-allowed transitions of N2 occur in the EUV (Ajello et al., 1989b). The excitation of the N2 RV states present in the EUV and FUV (80–140 nm) plays a role in establishing 781 UV Molecular Spectroscopy from Electron Impact for Astrophysics the physical composition of an N2-bearing atmosphere (Earth, Titan, Triton, and Pluto). The electronic transitions proceed from the X 1Σg+ ground state to nine closely spaced (12–15 eV) RV states, which are the source of the molecular emissions in the EUV observed by spacecraft (Ajello et al., 2007). Three of these RV states, b 1Πu, b′ 1Σu+, and c′4 1Σu+, are highly perturbed, weakly-to-strongly predissociated, and have significant emission cross sections (e.g., James et al., 1990). The other two RV states, c3 1Πu and o3 1Πu, are nearly 100% predissociated by the triplet C 3Σu+ and C′ 3Πu states (Lewis et al., 2005). When these five singlet-ungerade states predissociate, they eject fast N-atoms (>1 eV) through the N(4So) + N(2Do) and N(4So) + N(2Po) dissociation limits located at 12.1 and 13.3 eV, respectively. The energy level diagram of the RV states and the names of the emission band systems are shown in Figure 28.16. The emission spectrum of the singlet-ungerade RV states 125 1 + 1 Πu Σu 1.0 N2+ × 2Σu+ 1.2 b΄ 1Σu+ ν 28 27 26 25 24 23 22 21 20 19 18 17 16 15 14 13 12 11 10 9 8 7 6 5 4 3 2 1 0 b 1Πu ν 115 110 105 19 18 17 16 15 14 13 12 11 10 9 8 7 6 5 4 3 2 1 0 2 0 2 0 c41Πu c΄5 1Σu+ D +D 14 3 7 8 1 0 4 5 15 πuc31Πu σuc΄41Σu+ (N2+ A 2Πu)3sσgo 1Πu 10 11 2 4S0 +2P0 3p 16 17 13 4 1.8 1 b΄ 1Σu+ 13 b 1Πu S +2D0 12 4S0 +4S0 75 70 a 1Π g 9 3 2 0 10 8 LBH 65 High Rydberg– valence states of N2 Dissociation limits BHII 80 11 Carroll-Yoshino 85 Worley-Jenkins c-a 95 90 14 4 0 BHI Gaydon-Herman Energy (cm–1) 100 24 23 4p 1.6 Energy (eV) 120 1.4 1 X 1Σg+ 1 0.6 0.8 1.0 1.2 1.4 1.6 Internuclear distance (Å) 1.8 0 FIGURE 28.16 Partial energy-level diagram for N2 emphasizing the 12–15 eV energy region of the RV states. The right side of the figure shows the diabatic potential curve, and the left-hand side the observed vibrational levels. The circles and x’s in the figure are explained in Ajello et al. (1989b). 782 Charged Particle and Photon Interactions with Matter Table 28.2 The Cross Sections for Low Lying Five RV States of N2 State Qex (10–19 cm2) Qem (10–19 cm2) Qpre (10–19 cm2) Qfem (10–19 cm2) c′ Σ b′ Σ b 1Πu c3 1Πu o3 1Πu Totals 158a,b,d 128a,e 121a 161a 75a 643 125a,c,d 15.5a 6.1a 0a 0a 147 34a,b,c 112.5a,e 115a 161a 75a 497 122f 19.3f 8.4f 7.4f 5.7f 163f 1 + u 4 1 + u Note: Predissociation (fast N I atom) yield (Qpre /Qex) = 497/643 = 77% and EUV photon yield = 23% (Ajello et al., 2007, columns 2–4). a Where Q = Q ex em + Qpre. b v′ = 0 at 150 K, η (c ′ ) = 23%, at 300 K, η (c ′ ) = 26%, where η is predissociation yield. pre 4 pre 4 c Includes additional c ′ (0, v″ = 6–12) bands (Bishop et al., 2003; Ajello et al., 2007). 4 d Includes revised Q (v′ = 0) = 125 (units of 10−19 cm2). ex e b′ 1Σ + value based on correction to v′ = 9 and 11 emission cross sections (Walters et al., 1994; u Ajello et al., 2007). f Preliminary high resolution emission cross sections (Ajello, 2010) in column 5. displays many irregularities due to homogeneous RV interactions within the 1Σu+ and 1Πu manifolds and 1Σu+ ∼ 1Πu p-complex heterogeneous interactions (Liu et al., 2008). The recently revised emission cross sections of the highly perturbed b 1Πu, b′ 1Σu+, and c′4 1∑ u+ states that are weakly-tostrongly predissociated are large; the excitation, emission and predissociation cross sections for the low-lying five RV states are summarized in Table 28.2. Table 28.2 adapted from the work of Ajello et al., 2007, including minor changes, in columns 2 to 4, respectively; and the emission cross section from the recent higher resolution work of Ajello (2010) is given in column 5. Ever since the Voyager 1 (V1) encounter with Saturn in 1980, the EUV airglow of Titan has challenged attempts to explain both its spectral content and its excitation source. Because of the similarity to optically thin laboratory spectra from electron impact on N2 (Fischer et al., 1980; Ajello et al., 1989b), most early analyses of the V1 UVS data argued that Titan’s EUV airglow was dominated by the N 2 c 4′ 1∑ +u (0) → X 1∑ g+ (0) , i.e., c′4 (0, 0) band near 95.8 nm and the c′4 (0,1) band near 98 nm (Broadfoot et al., 1981a,b, Strobel and Shemansky, 1982). Though readily excited by photoelectron impact, the earliest work on the Titan airglow noted, however, that the resonant c′4 (0, 0) band was optically thick near peak photoelectron excitation. An excitation source driven by the Sun was therefore ruled out, since the c′4 (0, 0) emission band would be radiatively trapped, so a magnetospheric source near Titan’s exobase was proposed instead (Strobel and Shemansky, 1982). The issue was studied by Stevens et al. (1994), who developed a c′4 (0, v′′ ) multiple scattering model for the terrestrial atmosphere and showed that c′4 (0, 0) should be weak or undetectable near peak photoelectron excitation and that c′4 (0,1) should dominate over c′4 (0, 0). A similar analysis was done for Titan’s airglow by Stevens (2001, 2002) and Stevens et al. (2003), who argued that c′4 (0, 0) was misidentified at Titan and two prominent N I multiplets (95.2 and 96.4 nm) produced primarily by photodissociative ionization (PDI) of N2 were present instead. This meant that the Titan EUV dayglow could be excited exclusively by the Sun. The key N I emissions that could not be conclusively identified by UVS because of its low spectral resolution (3 nm) have now been identified with the higher spectral resolution (0.56 nm) of the UVIS instrument on the Cassini spacecraft. The UVIS disk-averaged dayglow spectrum in the spectral range 90–114 nm is shown in Figure 28.17 (top panel) at 0.56 nm FWHM. The 16 indicated dayglow features are identified in Table 28.3. The identifications are based on the work of Ajello et al. (1989b), James et al. (1990), and 783 UV Molecular Spectroscopy from Electron Impact for Astrophysics 1.0 December 13, 2004 Lab – c΄(0,0–2); 8.7 R N I and N II: 5.5 R c4΄(0,0–2): 1.6 R Composite: 17.5 R Day 0.8 0.6 12 0.4 3 4 5 6 7 8 9 10 11 12 13 14 15 16 0.2 0.0 0.2 Night 0.0 900 950 1000 1050 Wavelength (Å) 1100 FIGURE 28.17 (Top panel) Regression analysis to UVIS dayglow spectrum from December 13, 2004. The regression model fit consists of three independent vectors: (1) an optically thin 20 eV electron-impact lab fluorescence spectrum, with c′4 (0,0) dotted; (2) the calculated multiple scattered emergent spectrum of the c′4 (0,v″ = 0–2) progression transmitted through an optically thick medium; and (3) a spectrum of N I and N II emissions (Ajello et al., 2007). (Lower panel) Cassini UVIS nightglow spectrum. TABLE 28.3 Identification of Strongest Titan Dayglow Emission Features from Cassini UVIS on December 13, 2004 Feature λ (Å) 4πIb,c (R) Identificationa 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 909 915 928 944 953 965 980 987 1007 1026 1034 1054 1070 1086 1118 1135 0.50 0.32 0.41 1.56 0.84 1.39 1.47 1.45 1.46 1.71 0.46 0.56 0.33 2.31 0.51 1.33 c′(4,1), N(4S-4P), b′(16,2), b′(12,1) N(3P-3Po) b′(9,1), c′(6,4) c′(4,3), c′(3,2), b′(9,2), c′(6,5), b′(16,4) N(4So-4D), N(4So-4P) c′((1,1), N(4So-4P), c′(3,3), c′(4,4) c′(0,1) c′(3,4), c′(4,5), c′(6,7) c (′0,2), c′(3,5), c′(4,6), b(1,1), c′(6,8), b′(9,5) H Ly-β b(1,2), b′(9,6) N(2Do-2P), b′(11,7), b(1,3), b′(3,5) N(2Do-2,4D), N(2Do-2,4P) N+(3P-3Do) N(2Do-2D), N(2Do-2P), b′(9,9) N(4So-4P) Source: Ajello, J.M. et al., Geophys. Res. Lett., 34, L24204, 2007. a Identifications from Ajello et al. (1989b), James et al. (1990), Bishop and Feldman (2003), and unpublished high-resolution (0.2 Å FWHM) laboratory spectra. b Total observed EUV integrated disk intensity (900–1140 Å) in Rayleighs (R) is 16.6 R. c VI UVS: UVIS comparison; total observed UVIS intensity (920–1015 Å) is 8.6 R vs. total modeled VI intensity 920–1015 Å is 20.9 R. 784 Charged Particle and Photon Interactions with Matter unpublished, laboratory high-resolution spectra Ajello (2010), as well as the terrestrial airglow spectra of Bishop and Feldman (2003). Laboratory spectra (0.02 nm FWHM) have shown the presence of about 200 spectral features from electron-excited N2 over the same EUV spectral range (Ajello et al., 2009). On average, there are some 10 emissions for each feature number in Figure 28.17 (top panel); we list only the strong ones in Table 28.3. The strongest is feature number 14, the N II multio plet (3P-3D ) near 108.5 nm with an intensity of 2.3 Rayleigh (R). Whereas Voyager 1 only observed a few blended EUV features, the UVIS dayglow spectrum indicates 16 features, with the c′4 (0, 0) band conspicuous by its absence. For completeness, the nightglow spectrum is included in the lower panel of Figure 28.17. There have been no high-resolution (<0.01 nm FWHM) laboratory studies of the optically thin, electron-impact N2 fluorescence EUV spectrum from 50 to 120 nm since the medium-resolution (0.03 nm FWHM) study 20 years ago (Ajello et al., 1989b). ESL’s effort for higher resolution (FWHM ≈ 0.002–0.010 nm) studies is now underway. Our more recent high-resolution laboratory measurements have found a total of nine RV states contributing to the N2 EUV emission spectra from 80 to 140 nm; see Table 28.4 (Ajello, 2010). These states have principal quantum numbers through n = 6 and contribute to the emission and predissociation cross sections of N2 in the EUV. We show examples of high-resolution laboratory spectrum measured at ESL in Figures 28.18 and 28.19. Figure 28.18 shows the c′4 1∑ u+ (v′ = 0) → X 1∑ g+ (v′′ = 1) band model at 98 nm (Liu et al., 2008), the strongest band in the Titan EUV airglow (i.e., feature 7 in Figure 28.17a). The c′4 (0,1) band analysis was used to determine predissociation yields for each rotational level and a band transition moment. There are now full spectral models for the rotational structure of the c′4 1∑ +u (v′ = 0) → X 1∑ +g (v′′ = 0,1,2) progression at 95.9, 98.0, and 100.3 nm (Stevens, 2001; Liu et al., 2005, 2008) with which we can synthesize optically thick photoelectron-excited spectral lines using a multiple scattering model. Figure 28.19 shows a medium-resolution laboratory spectrum (0.02 nm FWHM) at both 20 and 100 eV compared to a Cassini EUV (90–115 nm) spectrum (dashed-line) indicating that there are many N2 bands (approximately 200) contributing to each of the observed 16 Cassini features in Table 28.3. At this point, it is necessary to study the rotational cross sections and predissociation yields of the strongest remaining vibrational band features identified in Table 28.3. TABLE 28.4 List of N2 Rydberg and Valence Electronic Band Systems Observed in EUV Spectra of Electron-Impact-Induced Fluorescence Electronic Transition Te (cm−1) b′ Σ → X Σ -valence b 1Πu → X 1Σg+-valence 104,498 101,675 104,519 1 + u 1 + g c ′4 3pσ 1Σu+ → X 1Σg+ Rydberg o3 3sσ 1Πu → X 1Σg+-core excited c 5′ 4pσ 1Σu+ → X 1Σg+ c6′ 5pσ 1Σu+ → X 1Σg+ c3 3pπ 1Πu → X 1Σg+ c4 4pπ 1Πu → X 1Σg+ c5 5pπ 1Πu → X 1Σg+ 105,869 115,876 — 104,476 115,636 — Source: Ajello, J.M. High resolution spectra of N2, 2010, in preparation. See Huber and Herzberg, 1979 for electronic energies of each state. 785 UV Molecular Spectroscopy from Electron Impact for Astrophysics 7000 P(13) 1000 P(12)b΄ P(14) P(15) P(16) P(17) P(18) P(19) P(20) P(10) P(9) P(7) P(11), P(12) P(8) P(6) P(4) P(5) P(2) P(3) R(3) R(2) P(1) 2000 R(0) 3000 (Δλ = 33 mÅ, E = 100 eV, T = 260 K) R(1) R(14–21); R(9)b΄ 4000 Observed Model R(10)b΄; R(7, 8, 9) R(6) R(5) R(4) 5000 R(10–13; 22, 23) 6000 Relative intensity (arb. units) c΄4 1Σu+ (0) – X 1Σ+ g (1) e + N2 0 –1000 979.9 980.1 980.3 980.5 980.7 980.9 Wavelength (Å) 981.1 981.3 981.5 FIGURE 28.18 Comparison of the high-resolution laboratory and close-coupled-Schrödinger spectral model for the c′4 (0)-X(1) transition rotational structure to obtain predissociation yields and diabatic transition moments (Liu et al., 2008). c΄(0,0) 0.3 0.0 c΄(2,2) 0.6 c΄(3,3) 955 960 965 b΄(11,4) 975 980 970 Wavelength (Å) c΄(6,7) b(1,0) c΄(2,3) 985 o3(1,3) N 0.9 –0.3 950 N b΄(12,5) c΄(1,1) N c΄(0,1) b΄(16,6) 1.5 c΄(3,4) c΄(4,5) N N c3(1,1) Relative intensity (arb. units) 20 eV N2 lab spectrum Cassini Titan December 13, 2004 N 1.8 1.2 100 eV N2 lab spectrum N c΄(1,2) 2.1 b΄(6,2) c΄(6,6) b΄(12,4) 2.4 b΄(11,5) b΄(18,7) 990 995 1000 FIGURE 28.19 Medium-resolution spectrum of e + N2 at 0.2 Å FWHM 100 eV and 0.6 Å FWHM at 20 eV compared to the Cassini UVIS spectrum of December 13, 2004 at 4 Å FWHM. The identification of the molecular and atomic features is from Ajello (2010). 786 Charged Particle and Photon Interactions with Matter Additionally, the low temperature of Titan’s atmosphere prompts the need for laboratory measurements of cross sections at low temperatures from 120 K found near the mesopause (500 km) to 186 K at the exobase at 1400 km (Wilson and Atreya, 2005). We have perfected expansion cooling of molecules through effusive nozzle for molecular-beam–electron-beam interaction to match Titan’s atmospheric temperatures (Ajello et al., 1998a) and intend to carry out such studies. 28.4.4 N2–FUV A variety of space missions have been flown to observe terrestrial N2 emissions in the FUV spectral regime. These include the MSX, TIMED, POLAR, IMAGE, and DMSP satellites. Moreover, solar UV spectral irradiance measurements, important for establishing the radiative energy input to the Earth’s upper atmosphere, are currently being obtained by instruments on board the TIMED and SORCE satellites. This suite of instruments allows the interaction between the Sun and the Earth to be studied in unprecedented detail over a solar cycle. The measurement goals of these missions are to achieve an accuracy of better than 10% in defining the atmospheric parameters (temperature, composition, density, etc.) on a global scale and to determine radiative, chemical, and dynamical energy sources. For remote sensing of the upper atmosphere, there are four principal wavelength intervals in UV imaging satellites that have been used to observe the distribution of N2 and O. Typical of these bands are those of the Global UltraViolet Imager (GUVI) instrument on TIMED: O I (130.4 nm), O I (135.6 nm), N2 (141– 153 nm), and N2 (167–181 nm). The latter two wavelength intervals are referred to as Lyman–Birge– Hopfield (LBH) short (LBHS) and LBH long (LBHL), respectively. They arise from the transition of N2 (a 1Πg → X 1Σg+). As an example, we show in Figure 28.20 an MSX FUV auroral spectrum (Paxton and Meng, 1999) with the LBH bands and atomic oxygen emissions indicated. Because of their importance in atmospheric remote sensing, we review the current understanding of LBH e­ xcitation and emission processes in some detail in this chapter. The analysis of the remote sensing spectra aimed at unraveling the behavior of the major constituents of the upper thermosphere, N2, O2, and O, and the auroral energy input depends on the details of the N2 LBH, and O emission cross sections, as well as the absorption cross section of O2. The fundamental excitation and emission processes involved for N2 and O and their cross section definitions are 1. e− (Ee) + N2 → e− (Ee − ΔEe) + N2* → e− + N2 + hν (a 1Πg − X 1Σg+) •• σex (LBH) is the cross section for direct excitation of the optically forbidden (τ ∼ 55 μs) a 1Πg − X 1Σg+ LBH band system from 120 to 210 nm, including LBHS (141–153 nm) and LBHL (167–181 nm). 2.e− (Ee) + N2 → e− (Ee − ΔEe) + N2* → e− + N2 + hν (a′ 1Σu and w 1Δu → a 1Πg) •• σcasc (LBH) for cascade emission from optically forbidden (τ > 1 ms) cascade transitions (a′ 1Σu and w 1Δu → a 1Πg) to the LBH band system. − 3.e (Ee) + O → e− (Ee − ΔEe) + O* → e− + O + hν (3P2 → 5S2o at 135.6 nm) •• σex for optically forbidden emission (τ ∼ 180 μs) of OI (135. 6 nm). 4.e− (Ee) + O → e− (Ee − ΔEe) + O* → e− + O + hν (3s 5S2o → 3p 5P1,2,3 and 3s 3S1o → 3p 3P0,1,2) •• σcasc (O I) for dipole-allowed hν (τ ∼ 1−10 ns) of O I (777.4 and 844.6 nm and higher order states). The history of LBH cross sections by electron-impact measurements was reviewed by van der Burgt et al. (1989) and (Meier, 1991). Shown in Table 28.5 are the N2 LBH cross section data reported in the literature. There are considerable differences among the cross sections, with values for direct excitation to the a-state differing by almost a factor of two in some cases. The discrepancies could be due to experimental limitations in fully capturing the long-lived emitting states, improper accounting of cascade contributions, or both. The shape of the excitation function peaking at about 18 eV was measured by Ajello and Shemansky (1985). This has been the standard cross section used in the 787 UV Molecular Spectroscopy from Electron Impact for Astrophysics SPIM1. Filter1. 40 × 272.2 Hz. mixed; 164/886; MP = 19 4000 SPIM2. Filter1. 40 × 272.2 Hz. mixed; 164/886; MP = 19 80 OI 130.4 nm OI 135.6 nm LBH S LBH L 3000 2000 60 40 1000 20 0 120 5 130 10 15 140 20 150 160 25 30 (a) 0 170 102 180 2 200 4 220 6 240 8 101 Polar LBH L image Ultraviolet imager 01 Mar 99 00:10:22 UT 12 60 Photon cm–2s–1 70 GC Alt 9.0 100 06:00 6 10 0 Geographic Lat/Lon 1.8 00:00 (b) 80 18 Apex MLat/MLT 12:00 18:00 23:59 FIGURE 28.20 (a) MSX FUV spectrum showing N2 LBH and OI multiplets (Fischer et al., 1980); (b) POLAR spacecraft image of LBH image. Note that for GUVI, the LBHL band covers 167–181 nm (Paxton and Meng, 1999). Aeronomy community since then. But recent remeasurements by Johnson et al. (2005b) and Young et al. (2010) found the peak nearer 20 eV, with a different energy function. The implications of the new measurement are discussed below. Strickland et al. (1995) have shown that satellite observations of the thermospheric ratio of O I 135.6 to N2 LBH are closely related to the O/N2 column density ratio, which itself is a good indicator of thermospheric dynamical conditions, especially during geomagnetic storms (Meier et al., 2005; Crowley and Meier, 2008). The N2 LBH cross sections of Ajello and Shemansky (1985 or AS85) have been extensively used in establishing this relationship. Various modelers have scaled the AS85 cross section by as much as a factor of 2 both to adjust for revisions in the absolute standard for the measurements of direct excitation to the a-state and to account for the estimated effects of cascade to the a-state from the a′ 1Σu and w 1Δu states (Meier, 2008). Because of the importance of the LBH cross section to remote sensing, we review the basis of Meier (2008) for estimating the best cross section to use until new measurements become available. AS85 obtained a value of 3.02 × 10 −17 cm2 at 18 eV for the peak excitation cross section from a model fit to the laboratory data (their Table 5a, column 2). They found that predissociation accounts 788 Charged Particle and Photon Interactions with Matter TABLE 28.5 Comparison of N2 LBH Cross Sections (in Units of 10 −17 cm2) Reference Ajello (1970) PE Brinkmann and Trajmar (1970) ES Cartwright (1977;1978) ES Ajello and Shemansky (1985) PE Mason and Newell (1987) MP Brunger and Teubner (1990) ES Eastes and Dentamaro (1996), Eastes (2000) model Budzien et al. (1994) Strickland et al. (2004) estimate Campbell et al. (2001) Johnson et al. (2005) EI Meier (2008) model analysis Young et al. (2010) Present estimate Cascade Contribution Estimates (% of Excitation) Peak Emission Cross Section, Including Cascades Estimate 73 Not observed 4.63 2.35 55 4.15 2.70 2.71 45 40 2.64 1.98 1.98 74 29–48 31 3.50 3.79 4.69 2.10 4.08 2.22–2.57 2.28 Peak Excitation Cross Section 3.85 4.50 2.72, 3.02a 2.65b 3.50 4.24 3.02 Note: PE: photoemission measurement, MP: metastable particle measurement, ES: electron scattering, EI: electron impact. a This value is the result of a scaling by a factor of 0.90 following the work of Trajmar et al. (1983). b This value is the result of a scaling by a factor of 0.875 due to the reevaluation of the H Lyman-α standard (van der Burgt et al., 1989). for a loss of 12.29% of all excitations to the a-state; the emission branching ratio for total emission is therefore 0.8771 (ignoring vibrational/rotational dependence). To calibrate their emission cross section measurements, AS85 used as their standard, the cross section for electron impact on H2 yielding H Lyman alpha. AS85 adopted a cross section of 0.818 × 10 −17 cm2 at 100 eV (or 0.578 × 10 −17 cm2 at 200 eV). More recently, Liu et al. (1998) measured an H2 Lyman alpha cross section of 0.716 × 10 −17 cm2 (near the value of 0.703 × 10 −17 cm2 recommended by McConkey et al. (2008) ). Consequently, we reduce the AS85 peak LBH excitation cross section to 2.64 × 10 −17 cm2 (=3.02 × 0.716/0.818). For emission without cascade, this becomes 2.64 × 10 −17 × B = 2.32 × 10 −17 cm2. Figure 28.21 shows the electron impact cross sections for excitation of a, a′, and w states. The scaled AS85 cross section is shown as a solid line, and the data of Young et al. are given by the individual points. The dashed line is a fit to the Young et al. data obtained by scaling and stretching the AS85 energy function. The Cartwright et al. (1977) a′ and w cross sections, often used for dayglow modeling (Strickland et al. 1999), are shown as solid lines. More recently, Johnson et al. (2005b) have remeasured these cross sections, finding them to be lower than Cartwright et al. Their data are plotted as asterisks. The dashed line is an attempt to fit the Young et al. data by adjusting the Cartwright et al. energy function. The dashed lines in Figure 28.21 do not fit the data very well for energies greater than about 60 eV, but they should be sufficiently accurate for dayglow modeling because the photoelectron fluxes peak at much lower energies. It has been known (at least) since the work of Freund (1972) that cascade takes place between the a 1Πg state and both the a′ 1Σu and w 1Δu states. Later evaluations of cascade were published by Cartwright (1977, 1978) and Eastes (2000). Both Cartwright and Eastes carried out detailed calculations of the interactions among the various states, including laddering back and forth, enhanced ground state vibrational populations, threshold effects, etc. Because a correct calculation of the a 1Πg 789 UV Molecular Spectroscopy from Electron Impact for Astrophysics Excitation cross section (cm2) 10–16 a-state a'-state w-state Cartwright Johnson et al. Fit AS85 scaled Young et al. Fit Cartwright Johnson et al. Fit 10–17 10–18 10–19 10 100 Energy (eV) 1000 10 100 Energy (eV) 1000 10 100 Energy (eV) 1000 FIGURE 28.21 Electron impact excitation cross sections relevant to the N2 Lyman-Birge-Hopfield band system (a 1Πg → Χ 1Σg+) in nitrogen atmospheres. Left panel: direct excitation to the a-state. Middle panel: excitation to the cascading a′-state. Right panel: excitation to the cascading w-state. See text for details. population rate, including interactions with the a′ 1Σu and w 1Δu states is very involved, it is useful to derive an effective emission cross section to correct the direct a 1Πg population rate for the effects of cascade. This has been a common approach where a fully developed cascade model is computationally prohibitive for routine processing of satellite databases. Because transitions of a′ and w to the X-state of N2 are forbidden, we assume that all excitations of these states end up as a-state emissions. The total volume emission rate from the a-state (ignoring the details of populating the individual vibrational states) can be written as the product of the excitation (population) rates and the branching ratio, B, for emission: a a a′ jem ( z) = Bjex ( z ) + Bjex ( z ) + Bjexw ( z ) (28.11) where j is the number of emissions (excitations) cm3/s and B is the branching ratio for emission (1 –the probability of predissociation). Equation 28.11 can be rewritten as j a ′ ( z) jexw ( z) a a jem ( z) = Bjex ( z ) 1 + ex + a a jex ( z) jex ( z) (28.12) If the a, a′, and w volume excitation rates have similar altitude dependences, the quantity in brackets is constant. (See below for more details on this assumption.) The direct volume excitation rate is the product of the excitation rate (g-factor) per second per molecule and the N2 number density, n: with the g-factor defined as jex ( z) = gex ( z )nN2 ( z ) ∫ gex ( z) = σ ex ( E )F ( E ) dE (28.13) (28.14) 790 Charged Particle and Photon Interactions with Matter where σex is the excitation cross section F is the photoelectron flux, both evaluated at energy, E The cross section can be written as the product of the peak cross section and ϕ, the normalized energy function: σ = σpeakϕ(E). Then ∫ peak gex ( z) = σ ex φ( E )F ( z, E ) dE = σ peak ex γ ( z ) (28.15) where γ(z) describes the altitude dependence of the g-factor. If γ is the same for excitation and emission (i.e., the energy functions are the same or the energy dependence of F does not change with altitude), then the a-state volume emission rate can be defined in a similar manner: ∫ a jem ( z) ≡ nN2( z)gem( z) = nN2( z) σaeff φ( E )F ( z, E ) dE = nN2( z)σaeff γ ( z) (28.16) where σaeff is defined as the effective peak cross section for emission from the a state, including cascade components. Substitution of Equations 28.13 through 28.16 into Equation 28.12 gives the following relationship for the effective emission cross section: j a ′ ( z ) jexw ( z) σaeff γ ( z )nN2( z ) = Bσaex γ ( z )nN2( z ) 1 + ex + a jex ( z ) jeax ( z) (28.17) j a ′ ( z ) jexw ( z ) σaeff = Bσaex 1 + ex + a a jex ( z ) jex (z) (28.18) or Next the Atmospheric Ultraviolet Radiance Integrated Code (AURIC; Strickland et al., 1999) model was used to calculate thermospheric volume excitation rates (without cascade) using the latest Young et al. (2010) and Johnson et al. (2005b) cross sections for a, a′ and w states at several solar activity and illumination conditions (Evans, 2010). We found that the ratios for a′/a and w/a (using shorthand notation for the ratios of volume excitation rates) are nearly independent of altitude between 150 and 250 km (to within ± 5%) where the bulk of the dayglow originates, and equal 0.134 and 0.172, respectively. Substituting these into Equation 18, the effective a-state emission cross section becomes σeff = 0.8771 × 1.98 × 10–17 cm2 × (1 + 0.134 + 0.174) = 1.74 × 10–17 cm2 × [1 + 0.31], or σeff = 2.28 × 10–17 cm2. Thus, our estimate indicates an a-state emission cross section enhancement of 31% by cascade. Our simplified estimate can be compared with the much more detailed calculations of Cartwright (1978) and Eastes (2000). Cartwright (1978) modeled the vibrational populations of a variety of N2 states in an IBC II Aurora. His direct a-state excitation cross section was 3.02 × 10 −17 cm2 (surprisingly the same as AS85). His Figure 28.18, left panel, displays the vibrational populations of the a-state for direct excitation and cascade from the a′- and w-states, for altitudes of 110 km and >130 km. Cartwright found little change in the percentage cascade contributions and fractional populations above 130 km, thereby supporting the assumption used in our derivation of the effective cross section. Using Cartwright’s >130 km case, we can estimate an effective emission cross section from his work. Summing the population rates for each vibrational level of the three states, we find total population rate ratios of a′/a = 0.60 and w/a = 0.13. The total is 0.73, more than twice our value, as expected from his larger cross sections. We obtain a similar value for the total cascade enhancement using the Trajmar et al. (1983) renormalization of the Cartwright cross sections, although the individual contributions from a′ and w are different. UV Molecular Spectroscopy from Electron Impact for Astrophysics 791 Eastes (2000) carried out a more detailed calculation of the LBH emission rate that included cascade. According to his Table 28.1 a peak excitation cross section of 2.69 was used. The conclusions of his paper state that the calculated emission rate with cascade is 55% larger than with excitation alone (i.e., without cascade). The effective cross section becomes 2.69 × 1.55 × 0.8771 = 3.66, somewhat larger than ours. But using the Johnson et al. a′ and w cross sections, his cascade would become 22% and the effective cross section becomes 2.9 × 10 –17 cm2, closer to our derived value. Cascade rates from a′- and w-states to the a-state shown in Figure 28.4 of Eastes (2000) vary strongly with altitude below about 200 km. This is discrepant with Cartwright (i.e., small variations above 130 km) and with the ratios of excitation rates from AURIC (although there may be some altitude-dependent effect in the cascade rates that could cause the emission rate ratios to differ from the excitation rate ratios). This discrepancy has not been resolved. A possible explanation is that Eastes used the Continuous-Slowing-Down photoelectron model of Jasperse (1976), whereas the AURIC photoelectron model is much more physically realistic. If the Jasperse model produces much greater altitude variations in the photoelectron flux energy dependence, it could account for the different behavior. Eastes also calculated the effect of collision-induced electronic transitions, but these should not be of much significance in the dayglow that is produced at higher altitudes where collisions are infrequent. Budzien et al. (1994) analyzed dayglow observations of the LBH band system. They used the AS85 excitation cross section corrected for the revised H2 standard (2.7 × 10 −17 cm2). They found that the total excitation rate had to be increased by a factor of 1.45, which when adjusted for predissociation, yields an effective emission cross section of 1.45 × 2.7 × 10 −17 × 0.8771 = 3.5 × 10 −17 cm2, larger than ours by 54%. Young et al. (2010) estimate the effect of cascade based on the ratios of cross sections: (a′ + w)/ a = 0.48 at 15 eV and 0.29 at 20 eV. Our value using volume emission rate ratios of 0.31 is quite close to their estimate. Their effective emission cross section is given in Table 28.5. In summary, we have made a simple estimate of the effective emission cross section that can be used to adjust the a-state excitation cross section for the effects of cascade from the a′- and w-states. Other determinations of the emission cross section based on either AS85 or Cartwright range are mostly higher than our derivation, because the more recent cross section measurements are lower than they used. Consequently, we recommend the use of σeff = 2.28 × 10 −17 cm2 at the peak at 20 eV as the effective LBH emission cross section to account for the effect of cascade into the a-state. Clearly, new measurements are needed to quantify the effect of cascade in the LBH system. As well, more modeling efforts are called for. Our estimate was based on a variety of simplifying assumptions and a single dayglow case. The work of Cartwright and Eastes needs to be repeated with more accurate photoelectron and auroral fluxes under a variety of geophysical and solar conditions. Another potential source of error in applying LBH cross sections to conditions where the energetic electron flux is changing rapidly with energy is the threshold effect. Thresholds for different vibrational levels are spread from 9 to 15 eV for the v″ = 0 → v′ manifold. With increasing electronimpact energy, the cross section for each vibrational level rises very steeply in the low-energy region where measurement uncertainties are generally large (Note that the Young et al. cross section data in Figure 24.21 are for the (3.0) vibrational transition.). Accurate laboratory measurements are needed near threshold energies using a high-resolution electron gun with electron beam energy spread of ΔEe ≈ 100 meV. Although this chapter focuses on molecular process, we digress briefly to consider the status of electron-impact excitation of atomic oxygen to the 5So state. The subsequent emission at 135.6 nm is used by aeronomers along with the LBH bands to measure the O/N2 column density in the thermosphere. Its absolute signal is a measure of the solar energy input to the atmosphere in the Earth’s dayglow. A literature review shows that there exists only one measurement (Stone and Zipf, 1974) and one theoretical calculation (Julienne and Davis, 1976) of OI 135.6 nm cross section of O reported more than 30 years ago and they differ by a factor of two. Meier (1991) scaled the Stone and Zipf measurement downward by a factor 0.36 to account for the improved determinations of the OI 792 Charged Particle and Photon Interactions with Matter 130.4 nm emission cross section that was measured simultaneously with that for 135.6 nm by Stone and Zipf. His recommended value for the peak cross section is 9 × 10 −18 cm2 at 16 eV. A validation of the old laboratory measurement of the emission cross section of O I (135.6 nm) is strongly needed as is an evaluation of the large cascade contributions. Since electron impact is the dominant excitation process in the dayglow and aurora, its cross section remains one of the outstanding missing parameters needed for reliable aeronomical remote sensing. Given the revision of the effective LBH emission cross section from that of AS85, the airglow algorithms need to be reconsidered. 28.4.5 CO As the most abundant interstellar molecule after H2, CO plays a very important role in the photochemistry of the ISM. The abundance ratio of CO to H2 is difficult to obtain from observations of the ISM, but can be determined from theoretical models. The models involve chemical reactions in which photodissociation by vacuum ultraviolet (VUV) radiation is the main destruction mechanism for CO, particularly in the range between 91.1 nm, the edge of atomic H absorption continuum, and 111.8 nm, which is the dissociation limit of CO into ground state atoms. The rate of photodissociation of CO by EUV radiation is one of the major uncertainties in these models. In view of these uncertainties and the importance of CO as a tracer molecule, a large number of experimental studies aimed at finding coincidences between CO molecular absorption lines and molecular hydrogen emission lines have been performed (Ciocca et al., 1997a,b). A large disparity in the values of the oscillator strengths of the A−X, B−X, C−X, and E−X exists in the literature. To resolve the discrepancies, we have carried out high-resolution EUV measurements of these states to determine predissociation yields and oscillator strengths (Ciocca et al, 1997a,b; Beegle et al., 1999). In Figure 28.22, we show for states we have studied, the potential energy diagram of Rydberg states lying above the A 1Π valence state. The internuclear distance of the minima in the potential curves of the Rydberg states overlies exactly the minima of the ground state, resulting in intense (0,0) bands. With a full-width-at-half-maximum (FWHM) of 0.0036 nm, we can resolve the rotational structure of the B(0,0), C(0,0), and E(0,0) bands. We show the rotational structure for these (0,0) diagonal bands in Figure 28.23. We also show a model of these bands. A simple model based on Honl-London factors (Ciocca et al., 1997a,b) and rotational constants matches the observed spectra. The predissociation yield of 88% is found for the E 1Π state, an average of 85% for the Π+ state, and 91% for the Π− state. The CO A−X band system emission spectrum has been observed in the airglow spectrum of Mars and Venus between 120 and 180 nm (Feldman et al., 2000). Longward of 125 nm, the UV spectra of both planets are dominated by the emission of CO fourth positive band system (A → X) and strong O I and C I multiplets. In addition, CO bands, B 1Σ+−X 1Σ+(0, 0) at 115.1 nm and C 1Σ+−X 1Σ+(0, 0) at 108.8 nm, are detected, and in the spectrum of Venus, there is a weak indication of the E 1Π−X 1Σ+(0, 0) band at 107.6 nm. The production mechanism of excited CO(A) molecules in the thermosphere is attributed to the photodissociation of CO2 by solar EUV shortward of 92 nm. The CO A−X band system is excited by the impact of photoelectrons and absorption of solar UV photons by both CO and CO2 (Barth et al., 1992). We have reported electron-impact-induced, medium-resolution fluorescence spectra (0.0031 and 0.00366 nm FWHM) of CO at 100 eV over the spectral region of 130–205 nm (Beegle et al., 1999). The features in the FUV emission spectra correspond to the fourth positive band system (A 1Π−X 1Σ+), atomic multiplets from C and O, and their ions. The absolute electronic transition moment was determined as a function of internuclear distance from relative band intensities. The excitation function of the (0,1) band (159.7 nm) was measured from electron impact in the energy range from threshold to 750 eV and placed on an absolute scale at 100 eV, as discussed in Section 28.3. The CO A–X band system emission cross section was established from a measurement of the relative band intensities at 100 eV. We have obtained high-resolution (∼0.0034 nm FWHM), second-order spectra of the A(0,1) band at 159.7 nm from CO by direct excitation and from CO2 by dissociative excitation. The fourth positive bands produced by dissociative excitation are significantly broader and hotter (300 K vs. 1400 K) than direct excitation at laboratory 793 UV Molecular Spectroscopy from Electron Impact for Astrophysics 12.0 E 1Π j 3Σ+ C 1Σ+ c 3Π Partial predissociation emission 11.0 1,3,5 – Σ E(0,0) 1.0 B(0,0) 10.0 b 3Σ+ Π 1,3,5Δ 1Σ+ C(0,0) eV C (3P) + O (3P) 1,3,5Σ+ 1,3,5 B CO No emission, >99% predissociation No predissociation 100% emission 4 3 2 1 0 0.8 X 1Σ+ 0 1.3 r (Å) 1.8 2.3 FIGURE 28.22 Simplified potential energy diagram for CO RV states (Ciocca et al., 1997). temperatures. A resolution of ∼0.2 nm of CO band structure is sufficient to distinguish the two types of excitation mechanisms in a planetary atmosphere of known thermospheric temperature. 28.4.6 SO2 Jupiter’s Io tenuous atmosphere is dominated by molecular SO2 and its dissociation products SO, S, O, and probable emissions from sulfur allotropes, Sx(S, S2, …). A detailed model of the auroral processes at Io requires, as a first step, a medium-resolution laboratory study of both Sx and SO2 as a function of energy to match the spectral dependencies of ground-based spectral observations (Bouchez et al., 2000), as well as the Galileo SSI observations of the blue Io auroral glow on E15 (Geissler et al., 1999). To date, Sx has not been successfully studied in the UV. Atomic and molecular data have been used most recently in the analysis of the Galileo Solid State Imaging observations of Io (Geissler et al., 1999), Cassini spacecraft observations of Io by the ISS (Porco et al., 2004; Geissler et al., 2004) and the UVIS (Esposito et al., 2005). The ISS is equipped with 15 filter combinations that span the wavelength range of 235–1100 nm. From the data acquired during the Jupiter Millennium Cassini encounter, Geissler et al. (2004) performed a detailed comparison of laboratory SO2 spectra with the Cassini ISS observations and inferred that a mixture of gases contribute to the equatorial glow. The equatorial glows were particularly bright in the near- UV wavelengths (230–500 nm) filters UV1, UV2, UV3, and Blue1. Based on the laboratory work of Ajello et al. (1992a,b), the relative emission intensities within each band pass confirm 794 Charged Particle and Photon Interactions with Matter 1.00 Q 1.00 1 + Data Model CO(B Σ ) + e hν0,0 ΔλFWHM = 36 mÅ 0.75 R1 R2 R0 P1 P2 0.50 0.25 0.75 Data Model ΔλFWHM = 36 mÅ 0.50 0.25 0 1149.2 1149.6 1150.0 1150.4 1150.8 1151.2 1151.6 1152.0 Wavelength (Å) 0.75 0.50 1 + CO (X Σ ) + e (100 eV) Q 1 + CO (C Σ ) + e hν0,0 1074.8 1075.6 1076.4 Wavelength (Å) 1077.2 1078.0 Data Model R2 Relative intensity (arb. units) 1.00 1074.0 ΔλFWHM = 36 mÅ R1 P2 1 CO (X 1Σ+) + e (75 eV) Q 1 CO (E Π) + e hν0,0 R0P1 Relative intensity (arb. units) CO(X 1Σ+) + e (30 eV) Relative intensity (arb. units) 1.25 0.25 0 1086.5 1087.0 1087.5 1088.0 1088.5 Wavelength (Å) 1089.0 1089.5 FIGURE 28.23 High-resolution EUV spectra of CO (B,C,E → X) (0,0) bands: data(solid) and model (dash). The FWHM is 36 mÅ (Ciocca et al., 1997). Relative intensity (arb. units) Laboratory MUV spectrum of electron excited SO2 2 SO (A – X) 98 eV 18 eV 8 eV Filter UV1 UV2 UV3 BL1 BL2 GRN Cassini ISS filters Center FWHM nm 255 40 300 60 340 70 445 105 440 30 562 145 Filter UV1 UV2 UV3 BL1 GRN Electron energy 8 eV 18 eV 98 eV 0.3 0.0 0.34 0.41 0.33 0.42 1.00 1.00 1.00 0.27 0.39 0.79 0.29 0.20 0.97 1 0 SO2 (A, B, α – X) –1 200 240 280 320 360 400 440 480 520 560 600 Wavelength (nm) Intensity ISS <1.0 (SO2) 0.30 (SO2) 1.00 0.93 (S2?) 0.96 (O, Na?) FIGURE 28.24 The calibrated SO2 electron-impact-induced fluorescence spectra were obtained at 8, 18, and 98 eV electron-impact energy and a spectral resolution of 1.8 nm over the wavelength range 200–600 nm. The two tables present the Cassini ISS filter band passes and the fraction of electron-impact-induced fluorescence of SO2 emission signal expected in each filter band pass normalized to unity at filter UV3 (Geissler et al., 2004; Ajello et al., 2002b). 795 UV Molecular Spectroscopy from Electron Impact for Astrophysics the presence of molecular SO2 in the Io atmosphere. The laboratory SO2 electron-impact-induced fluorescence spectrum is shown in Figure 28.24 along with a table that lists the UV, middle UV, and visible filters, and a comparison of the laboratory relative intensities at 8, 18, and 98 eV normalized to UV3 intensities. There is an agreement between the measured output of 100 kR from filter UV3 and the 8 and 18 eV relative intensities within the same band-pass, e.g., the laboratory peak intensity at 320 nm agrees closely with the UV3 filter centered at nearly the same wavelength. There is a Blue1 discrepancy and Green elevated due to the possible atomic emissions indicated in the table. The laboratory work of Ajello et al. (2002b) used in the Cassini ISS comparison only covered the wavelength range of 200–600 nm. Most of the ISS filters from the blue to the near-IR (500–1200 nm) range show substantial emission intensities as well. We have recently expanded our wavelength coverage to include the entire range of 200–1100 nm using newly acquired laboratory spectroscopic instrumentation that closely matches the Cassini ISS wavelength capability (Ajello et al., 2008). This added coverage is the first study of SO2 from the UV, visible, optical to near-IR range, i.e., the entire VOIR, which is needed to confirm the model analysis of Geissler et al. (2004). The Cassini spacecraft at Io and Jupiter during the Cassini Campaign has repeated a spectacular series of visible/near-IR auroral observations similar to those obtained by Galileo SSI but at improved spectral resolution. We show in Figure 28.25 the initial multi-spectral image of Io (a) (b) Tvashtar plume Pillan Pele To Jupiter (c) (d) FIGURE 28.25 Multispectral Image of Io during eclipse of January 1, 2001. (a) False color composite made up of IR4, CB1, and UV3 filter-images portrayed in color in the original work of Geissler et al. 2004 as red, green and blue, respectively. We portray the multi-spectral image in a grey scale with the small circular volcanic feature in right-center from Pele as ‘red’ IR4, outer ansa and circular limb glow is mostly ‘green’ UV3, inner ansa glow is ‘blue’ CB1. (b) CB1 (red) and UV3 (blue) images superposed on clear filter image. (c) Location reference map with grid lines at 30 degree intervals. (d) Annotated clear-filter image showing locations of volcanoes and plume glows discussed (Geissler et al., 2004). Charged Particle and Photon Interactions with Matter FOS G13OH counts/s 796 0.3 Io in sunlight 0.2 S S,O O S ~1–2 kR 0.1 0.0 1200 0.06 FOS G13OH counts/s S 1300 1400 Wavelength (Å) 1500 Io in shadow S S,O O 0.04 S S ~300 R 0.02 0.00 1200 1300 1400 1500 Wavelength (Å) FIGURE 28.26 Voyager visible image of Io by HST showing an active volcano and HST GHRS FUV spectrum of Io with tick marks at strong atomic emission lines of sulfur and oxygen (Clarke et al., 1998). obtained during the eclipse of January 1, 2002 showing a false color composite of the equatorial and limb emissions (Geissler et al., 2004). Besides being a scientific destination in its own right (Galileo and JUNO), Jupiter is used for gravitational assist trajectories to the outer solar system (e.g., the Cassini and New Horizons missions). Consequently, UV observations of the Jovian system are also taking place periodically as secondary mission objectives. Active magnetospheres are coupled to the ionospheres of the giant planets’ systems and produce particle-excited aurora and airglow. Trapped particle impact on a planetary satellite atmosphere can result in global excitation, both day and night. For Io, having a volcanically generated SO2 atmosphere, dissociative excitation by the magnetospheric Jovian plasma torus results in excited SO, S, and O, in addition to excited SO2 and ions, all of which emit radiation. It is believed that the bulk of Io’s atomic emission is powered by electron excitation of neutral S and O directly, rather than by the electron dissociative excitation of SO2 (Ballester et al., 1996). A visible image of Io is shown in Figure 28.26 along with an HST/GHRS spectrum in the FUV with spectral identifications (Ajello et al., 1992a,b; Clarke et al., 1994). There is an evidence, however, that both direct excitation of S and O and dissociative processes upon SO2 contribute to the Io emission spectrum: (1) Oliversen et al. (2001) indicate that short-term fluctuations in the O I 630 nm intensity is the evidence for a high-energy, nonthermal plasma tail (∼30 eV) for a one-step process, and (2) Ballester (1998) indicates that neither electron excitation of O I nor electron dissociative excitation of SO2 alone by plasma electrons can explain the HST or IUE observations. 28.5 Conclusions UV emission spectroscopy by electron-impact-induced fluorescence has been reviewed for a few molecules of major importance to astronomy and planetary atmospheres. The laboratory goals are to (1) measure electron-impact emission cross sections (0–2 keV) and fluorescence spectra (50–300 nm) for important atoms and molecules key to remote sensing observations of FUSE UV Molecular Spectroscopy from Electron Impact for Astrophysics 797 (Far Ultraviolet Explorer), HST (Hubble Space Telescope), HUT (Hopkins Ultraviolet Telescope), TIMED (Thermosphere Ionosphere Mesosphere Energetics and Dynamics), Galileo, Cassini, and many other spacecrafts; (2) emphasize recently observed and relevant UV transitions of cosmically abundant species of Jovian and terrestrial planetary systems, ISM, and comets (e.g., H, H2, HD, N2, SO2, O, CO, and O2); (3) provide collision strengths in analytical form or tables of cross sections for UV radiative processes for electron energy loss transport codes and for comparison to ab initio calculations; and (4) study corresponding VOIR cascade transitions (300–1100 nm or 1–5 eV excitation energy). A summary of salient planetary observation results from recent studies of the important atoms and molecules employing the ESL database are listed below: • The first analysis of the Cassini UVIS observations of the Saturn H2 aurora (Esposito et al., 2005) and the first analysis of the Jupiter millennium H2 aurora observations (Ajello et al., 2005a). • The first analysis of the Cassini Io visible aurora observations of predominantly SO2 by the ISS (Geissler et al., 2004). • The development of atomic and molecular hydrogen models used in the interpretation of low-resolution Galileo spectra, medium-resolution HUT spectra, and high-resolution FUSE and HST UV spectra of Jupiter (Dols et al., 2000; Ajello et al., 2002a, 2005a; Gustin et al., 2002, 2004). • The analysis of Galileo Solid State Imaging (SSI) H2 VOIR observations of Jupiter (Vasavada et al., 1999). • The modeling of Cassini and STIS/GHRS (Goddard High Resolution Spectrometer) UV observations of Io, Europa, and Ganymede (Trafton et al., 2007; Noren et al., 2001a,b; Vatti Palle et al., 2004; Hansen et al., 2005). • Resolved longstanding V1 UVS ambiguity on Titan EUV spectral content showing that the N2 Carroll-Yoshino c′4 (0,0) band (Broadfoot et al., 1981b) was undetectable and N I photodissociative ionization (PDI) multiplets were present instead (Ajello et al., 2007; Stevens et al., 1994). 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