*o* ' s ,, ,,, .' i 14-g 36-412 , m^ > ROO ;_' ' k ';, . THE MICROWAVE SPECTRUM OF KETENE H. R. JOHNSON M. W. P. STRANDBERG Lfl 0i'Y TECHNICAL REPORT NO. 192 4' MARCH 14, 1951 RESEARCH LABORATORY OF ELECTRONICS MASSACHUSETTS INSTITUTE OF TECHNOLOGY CAMBRIDGE, MASSACHUSETTS 1----111 ---_1_--- - -·II- The research reported in this document was made possible through support extended the Massachusetts Institute of Technology, Research Laboratory of Electronics, jointly by the Army Signal Cornps. the Navy Department (Office of Naval Research) ment of the Army Project No. 3-99-10-022. C MASSACHUSETTS INSTITUTE OF TECHNOLOGY RESEARCH LABORATORY OF ELECTRONICS March 14, 1951 Technical Report No. 192 THE MICROWAVE SPECTRUM OF KETENE H. R. Johnson M. W. P. Strandberg Abstract 1 2 1 12 16 HD C 12 1 6 , HD C 2 , The microwave absorption spectra of the ketene molecules H 2 C 2 0 2 12 16 e . and DC 2 0 have been investigated. Reciprocal moments of inertia have been determined for each from the measurements. The centrifugal distortion theory of Hillger and Strandberg has been found valid for both Q and R branches. The structure has been cal- culated and dipole moment measured; results check and extend the accuracy of values previously determined by other methods. Intensities of satellites of the lightest molecule corresponding to the lowest three vibrational fundamentals have also been measured, and changes in the average reciprocal moments determined. The vibrational frequencies have been calculated and found different from values reported in the literature by infrared workers. References and suggestions for further work are given. II^_II _PLIY-^III II^ _ ____ _ THE MICROWAVE SPECTRUM OF KETENE Introduction A. General Properties Ketene is an organic compound, CH 2 C=O, which at room temperature is a color- less, heavy, extremely poisonous (1) gas (Fig. 5). approximately -50°C. perature. It melts at -151°C and boils at Ketene is chemically reactive and a dimer exists at room tem- There is a large body of literature on the molecule, bearing mainly on its chemical properties. Because its spectrum is difficult enough to be interesting but perhaps simple enough to be precisely analyzed, considerable spectroscopic work has been published. Ketene has C2v symmetry and an electric dipole moment, and is nearly a prolate symmetric rotor. B. Early Microwave History Early in 1948, J. Goldstein of Harvard located four microwave rotational absorp- tion lines of ketene in the 20, 000-Mc/sec region, where the J = 0-"J = 1 transition would be expected on the basis of the known structure. At his request, the precise frequen- cies of those lines were measured in this laboratory, and the Stark coefficients were determined. The higher frequency transitions J = 1-2 and J = 2-'3 were also measured since our laboratory was equipped to work in those regions (40, 000 and 60, 000 Mc/sec respectively). Early in 1950, Bak and co-workers at Copenhagen measured the J = 0-1 of 1 1216 2 1 12 16 2 12 16 H 2C2 0 , D H C 2 0 , and D 2 C 2 0 (hereafter briefly referred to as H 2 C 2 0, DHC 2O and D 2 C 2 0 respectively) as well as some vibrational satellites (10). The reported absorption frequencies (wavemeter accuracy) check fairly well with our measurements, although some discrepancies amount to 20 Mc/sec. A preliminary report of our work herein described has been given (11). C. Reason for Interest The values of the three moments of inertia of H 2 C 2 0 would enable calculation of thermodynamic gas functions of possible engineering interest; also using those of D 2 C 2 0 the structure of ketene could be calculated; the combination of Q and R branch transitions that occur would give an interesting check on the theory of centrifugal distortion in asymmetric tops developed in this laboratory (12, 13); the relative intensities of the vibrational satellites which occur would help in the correct assignment of the fundamental vibrational frequencies; and the measurement of the Stark effect would enable accurate evaluation of the dipole moment independent of impurities. Consequently intensive work has recently been begun in this laboratory. I. Experimental Work A. Preparation of Ketene and Heavy Ketene Ketene was made by pyrolysis of acetone using a lamp described by Williams and Hurd (14). Their method was modified in that a vacuum system was used to minimize -1- ___II _ LII ·I -0 i-- 5 o cr re r~~~~~~~~~~ U) .U rl ct in (1) a) Us 9) 0 a) 01 be *, 0 Q1 En a (n -4- 4~~ bb FrH -( mmmn T srrrt .z_ -- -2- p - I loss of the deuterium compounds. With reference to Fig. 1, acetone was cracked at about atmospheric pressure in subsystem ADCB, and products bled off through capillary F to liquid nitrogen cooled traps GH and rotary vacuum pump I. A was surrounded by a water bath at 55 °C. Acetone in bulb Vapors rising from A cannot pass the drop condensed in constriction B, so they rise into D and make contact with the dull-red hot nichrome filament there. Most of the acetone is returned by the water-cooled condensers C and E to A; ketene, some acetone, and other products pass through capillary F (1 meter long, 0. 4 mm bore) into large cold traps G and H; the pressure on this side of the capillary is low enough so that the two traps are essentially 100 percent effective in condensing ketene and less volatile compounds (the second trap condenses very little). The pump removes at least some of a more volatile product, probably CH 4 . Purification of the ketene is carried out by fractional distillation in the following way. The substance is first triple-distilled at the temperature of dry ice in acetone. This removes impurities, mainly acetone, less volatile than ketene; they are returned to A for recycling. warmed. The ketene is then placed in a microwave spectroscope and slowly The absorption of the effluent vapor at the frequency of the J = 0--1 line is monitored as the vapor is being pumped off. When the spectroscope indicates ketene, and the absorption shows little increase with time, the pump is shut off. This results in discarding more volatile impurities, roughly 5 to 20 percent of the mixture. The ketene has been stored in vacuum for months at liquid nitrogen temperatures with no deterioration; some decomposition is noticeable in a week of storage at dry-ice acetone temperatures. Heavy ketene was made in the same way as the light, but 1. 5 cc of 96 percent pure heavy acetone, supplied to us by R. C. Lord of M.I,T. was used. DHC 2O was made from a mixture of 50 percent each of heavy and light acetones (attempts to make it by exchange of light ketene and heavy water were unsuccessful). B. Systems Used The spectroscope used for most of this work (15) employed square-wave Stark modulation at 6 kc/sec, and a 6 kc/sec amplifier, phase detector, and remodulator. The system bandwidth was roughly 10 cps. this system. Reflex klystrons were used as sources on Its ultimate sensitivity, used with a two-meter X-band cell of the usual type, appeared to be between 1 and 510 -8 cm -1 . A one-meter K-band Stark cell was used when the system was operated at frequencies above 30, 000 Mc/sec. Measurements in the vicinity of 60, 000 Mc/sec and initial measurements at 40, 000 Mc/sec were made with a direct absorption (no Stark) doubling system with superheterodyne detection, using an X-band cell ten meters long. C. Observed Spectrum Table I shows the observed frequencies of the three molecules studied, namely H 2 C 2 0, DHC 2 O, and D 2 C 2 0. Lines were identified by Stark effect, intensity and fre- quency. The identification given is thought to be the only one possible. Figure 2 shows log intensity plotted against log frequency for the lines of D 2 C 2 O. Neither instability -3- ____1__1_111_111_1- - _____1_1· I IE 0 =2 z z 2 i IU 7 8 9 0 12 15 20 25 30 40 FREQUENCY -KILOMEGACYCLES 50 60 80 100 Fig. 2 Spectrum of DZC 1 2 l6 nor dimerization of the sample was serious enough to render the microwave measurements difficult; nevertheless, effects which could be assigned to these actions were observed. In a brass waveguide at room temperature, after ten microns of ketene pres- sure had been maintained for some time, there was a decrease in peak line intensity of a factor of two in a few hours with an associated drop in Pirani gauge reading. When the waveguide was surrounded by dry ice, the intensity and pressure seemed even more stable. Furthermore, and fortunately for intensity measurement, if at room tempera- ture the pressure were initially high enough (>100. microns) to broaden the line considerably, the peak intensity would not change as the pressure dropped. that the remaining gas was at least 80 percent pure after an hour. This indicates These observations, however, are essentially only approximate. D. Relative Intensity Measurement To obtain the vibration frequencies, we measured relative intensities of the J = 0-1 transitions in ground and excited vibrational states. With reference to Figs. 4 and 5, the method used was to inject into the 6-kc/sec amplifier of the Stark spectrograph a -4- PI INTENSITY MEASURING EQUIPMENT //////// 6-KC STARK SQUARE WAVE GENERATOR REFERENCE ! I - - I- VARIABLE ATTENUATOR 1 SX/, ///// 7/ I// PHASE . SHIFTER X VOLTMIETER /Z// Z / |HIGH VOLTAGE -L///l/- ,! /1 /I /I i /I / _ KLYSTRON WAVEGUIDE WAVEGUIDE I . - I~~~~~~~~~~~~~~~~~~~~~~~~~ I 6-KC_ \_ HORIZONTAL t SAWTOOTH IGENERATOR ERTICAL IAMPLIFIER L, SIGNL CRO | Fig. 3 Block diagram of connection of intensity measuring equipment to Stark system. r V ARIARiF INI I OUTPUT _- i L I BALLANTINE VOLTMETER I PHASE SHIFTER -… Fig. 4 Detailed diagram of intensity measuring equipment. signal 180 out of phase with the 6-kc/sec signal from the detector crystal, and adjust the amplitude of this added voltage to exactly balance out the peak gas absorption signal. The only factor limiting the precision of this procedure appears to be the presence of noise. The amplitude uncertainty is roughly equal to the noise voltage present, so the percentage error in the ratio of ground-state to satellite line is smaller the greater the signal-to-noise ratio of the line. The results of about ten independent determinations of the intensity ratio at 27 ° C yield the result that the intensities of the four lines in the J = 0- 1 region of H 2 C 2 O are in the ratio 1:(0. 295 + 7 percent):(0. 205 + 10 percent):(0. 121 + 15 percent). These errors are limits within which the true intensity ratio is expected to fall. II. Interpretation of Absorption Frequencies A. General The rotational spectrum of a molecule is, to a good first approximation, that of a Because of the high resolution of microwave techniques, relatively small perturbing effects of rotation-vibration interaction must also be considered (16). The rigid rotor. terms "zero-point vibration correction" and "centrifugal distortion correction" are given to those parts of the effect of vibration on rotation which depend on vibrational -5- __--.-_111_----.--- -.11 ·---I- I I and rotational quantum numbers respectively (there is also a small constant vibrationrotation interaction term). In addition, rotation-electronic interaction occurs. These terms are generally very small because of the large mass ratio between electrons and nuclei. B. Rigid Rotor The rigid rotor frequencies were calculated by the methods of King, Hainer and Their power series in 6 was used for the R branch, and for Q branch lines Cross (17). with K_1 = 1; their continued fraction expansion was used for Q branch lines with K_1 = 2. C. Centrifugal Distortion The centrifugal distortion correction to the rigid rotor is the only one necessary for reasonable prediction of the whole microwave spectrum in terms of a selected set of The lines, since the other corrections are independent of rotational quantum numbers. problem of making this correction for asymmetric rotors has been treated by Lawrance There are six "centrifugal and Strandberg (12), and by Hillger and Strandberg (13). distortion constants" related to the structure of the molecule and the vibrational fundamentals. and R (AK there are general formulas for Q (K For molecules with 6<<1, 1 =0, 1= , J = 0) J =+1) branches (1) i= J (J+1) fl (K_1) + f 2 (K-1 ) Q branch: Vrigid R branch: Vdist dis rigi d (J+1)2 2 4 D J + K 2 1 DJK T (2) (2) Here, vrigid is the absorption frequency of the rigid rotor; vdist is the frequency correction to be added to vrigid to get Vmeas; Vmeas is the actual measured absorption frequency; D and DJK are two centrifugal distortion constants. fl (K 1) and f 2 (K 1), used here temporarily for purposes of discussion, contain the other four centrifugal distortion constants. A considerable amount of numerical calculation is involved in determining the six centrifugal distortion constants from the vibrational fundamentals. In view of some uncertainty in the assignment of these fundamentals for ketene, we will instead fit the microwave data to Eqs. 1 and 2. The fit was attempted in the following way for Q branch lines with K_ 1 = 1: for 6<<1l Vrigid = k (b-c) (3) where k is a constant involving 6 only in second and higher powers, and b and c are the usual reciprocal moments of inertia. Suppose that an approximate value of (b-c) is used to calculate vrigid; we will designate approximate quantities with primes. (b-c) = (b-c)' -6- (+a) Then let (4) whence Vrigid (l+a) =rigid (5) where a is the fractional correction by which (b-c)' is in error. Then vrigid = k (b-c)' (+a) (6) whence V -V meas I = J (J+1) fl (1) rigid f2 (1)+ (7) . Vrigid From Eqs. 1 and 3, this means that when a value (b-c)' is assumed and the left-hand side of Eq. 7 is plotted against J (J+i), a straight line should result. mentally found true. This is experi- The slope of the line is fl (1) and the intercept is [f 2 (1) + a] or a combination of J-independent centrifugal distortion and the necessary fractional correction to the assumed (b-c)'. Similarly treating the K 1> 2 lines of the Q branch, we may assume a value 6' as a first approximation to the true value 6 of the asymmetry Vrigid = (K 1) 6 K-1 -1 (8) where j (K_ 1) is a constant involving J and (b-c) but involving 6 only as a first-order correction. Writing 6 = 6' (1+P) where (9) is the necessary fractional correction to the estimated value 6', we get Vmeas rigid) w'as rigid = J (J+) Vrigid f (K) + + f (K f 1 ) (K-) + (10) (K -l-) ( 0) Again, this means that when a value of 6' is assumed and the left-hand side of Eq. 10 plotted against J (J+1), a straight line should result. for K_ 1 = 2 with DzCzO K 1 and HDCzO. This is experimentally verified The intercept of the K 1 = 3 line as well as the = 2 and K_ 1 = 1 plots would be required, however, to obtain f 2 and p. Unfortunately, only for D 2 C O 2 would such lines be strong enough to be detected, and none of the latter were searched for. The effect of this situation is to introduce uncertainty into the values of (b-c) and 6 extrapolated to zero centrifugal distortion of about 1:5000 and 1:1000 respectively; fortunately, the amount of this uncertainty is smaller than the uncertainty in the equilibrium moments of inertia caused by zero-point vibration, and hence has no effect on the accuracy of the structure determination. The limits of error given above are suggested by a definite deviation from linearity in the case of D 2 CzO of the plot of Eq. 10 for K_1= 2 when a change of 1:1000 in 6 is made; f 2 (2) was estimated in this way. fitting process described was carried out by least squares. -7- ---- ·------ ------------ `-- The Values of effective (b-c) and 6 in the ground vibrational state as well as measured centrifugal distortion constants are given in Table II. The number of significant figures given is much greater than the quoted error because of their empirical value for prediction of lines with K 1 < 2. R branch lines pose less of a problem. tional state. First we consider lines in the ground vibra- values of (b-c) and 6 found from the Q branch lines were For Hz2 C0, assumed correct, and DJ, DJK and (b+c) solved for from the many observed R branch lines by the method of least squares. searched for. For Dz2 C0, no lines of the group J = 2-3 were D = 0 was assumed since otherwise it calculated to be a small negative value with an uncertainty greater than its absolute value. transition was measured, so calculation of D For DHC20, only the J = 0-1 and DJK is impossible. This frequency is listed as (b+c). D. Zero-Point Vibration There are two well-known methods for finding the equilibrium moments of inertia from the microwave "effective" values, the first from vibrational data and the second from microwave data. In the calculations of the first method, anharmonic force con- stants which are generally unknown contribute effects of the same order as harmonic force constants so the calculation is seldom feasible. monic correction cn Rough calculations of the har- be used to calculate the order of magnitude of the error, however. This idea is later applied to calculation of the error to be assigned to the structure determination. The second method consists of finding rotational transitions of the mole- cule in each of the fundamental excited vibrational states. The reciprocal moment a for ketene in a vibrational state characterized by vibrational quantum numbers nl, n 2, ... n9 is then 9 a(n1 , n 2, ... n 9 )= a(, 0, .. 0) + a (ni + ) (11 i=l and similarly for b and c. Here the a are interaction constants and a(O, 0, ... 0) is the equilibrium reciprocal moment of inertia, which'can then be calculated. A considerable number of R branch lines of the molecule in excited vibrational states was found. For the J = 0-1 transition of H CzO, all but one of the interaction lines from vibrations v 7 , v 8 and v 9 were measured, enabling calculation of ab, ab, 8c9 ac8 ab and a c as well as DJK for each state. Since we have no knowledge of the other a values, however, we cannot correct for zero-point vibration. The known values are nevertheless interesting since they give the order of magnitude of this correction. The measured values of a and DJK are listed in Table II. E. Electronic Interaction There is a small effect on the rotation spectrum caused by the coupling of the elec- tronic motion to the rotation. Recent work by Eshbach and Strandberg (18) has shown how this coupling gives rise to a molecular magnetic moment which can be measured. -8- _ _ _ _ I We shall now show that the magnetic moment can be used to obtain the effect of the electronic interaction on the rotational frequencies. The hamiltonian of the rigid rotor plus the electrons is (negligible error in calculating the electronic interaction is made here by omitting the vibrational part) H=H +He+H' (12) where P Hr--Z i1 (13) i=a, b, c He = E iI Z j + Pij (14) V (a,b, c) i=a, b, c z, H'=- TL (15) 1 i=a, b, c Here N a , Nb, N c are the components of the nuclear angular momentum N resolved along the nuclear a, b and c principal axes of inertia; Ia, moments of inertia of the nuclear system; Ib' I c are the principal m is the mass of the electron; PajI Pbj' electron in a space-fixed Pcj are the components of linear momentum of the j system, resolved along the axes a, b and c; and V (a,b, c) is the potential energy of the electrons. The terms in L2/2I, etc. have been neglected. Shift in the center of a mass has also been neglected. Also (16) P =N + L where Pa, Pb' Pc are the components of the total angular momentum P of the electrons plus nuclei in a space-fixed system resolved along a, b, c; L a , L b , Lc are the components of the angular momentum L of the electrons in a space-fixed system resolved along a, b, c. Choose now the matrix representation in which P , He simultaneously diagonal. ' and H r are This can be done since these operators mutually commute (18). The eigenvalues of H r are the first approximation to the energy levels of the rotational The subscript n labels the eigenvalues En and eigenfunctions n of H e with n = 0 corresponding to the lowest state. H' is a small coupling between H e and H r which will influence the energy of each rotational level. After diagonalizing H in n by secondspectrum. order perturbation theory, the n=O elements of H are found to be H=- ,=I 1 I Aij (17) where -9- _-i·_---I ·- --- <oILjIn> <nILj o> E -E n o -E n Aij (18) In these and later equations, indices i, j and k run over a, b and c. We define A.. + A.. i l I. 3 e Gij =-7mc (19) and a symmetric tensor Gij cyclical in a, b, c of which typical elements are n e aa ZZk (bk+ - -= a Ck) k (20) and n ab - e eb - I Zk k ak bk Eshbach and Strandberg (18) showed for 1E states that if m i is the component of the along a principal inertial axis i vector rotational magnetic moment m i (21) =GijPj j where G = G e +G. n ij ij ij (22) Here, e is the electronic charge; v is the velocity of light; ak, bk and ck are the coordinates of the k t h nucleus in the principal inertial axis system; and Zk is the atomic th number of the k t h nucleus. If Aij=Aji, Eq. 17 can be written 1] ii PL H H =Z/ 7 1/ L jZz~P.P. - , 1= i i +Aj (A - (23) 2 i A sufficient condition for this assumption is that Gij be diagonal. With Eqs. 19 and 22, Eq. 23 becomes P2 H = mv i i I mv iiGnj ij P.P. '\i' ij 1 + mm eT i i G j (24) 1 The second term of the right-hand side of Eq. 24 can be written, using Eq. 20, as -10- i i i j (25) . 13 ~ 1 where typical elements of the tensor I e1j ,' symmetric and cyclic in a, b, c, are e 1 2 2 m Z k (bk + Ck) Iaa k e Iab Zb ,m Zk akbk . 7=Z k That is, ij is the moment of inertia tensor of the 'electrons considered concentrated at ij their respective nuclei, in the nuclear principal axis system. Using Eqs. 24 and 25, we have 2 IiiUi. e [PPi G..i i j where ij is the usual Kronecker delta. (26) 1e j The quantity in the brackets in Eq. 26 is obvi- ously the reciprocal of a moment of inertia tensor; we will now find the corresponding moment of inertia tensor. The bracketed quantity is nearly diagonal, so its reciprocal will be of the form ij 6 ij where Pij << Ik for all i, j, k. ij (27) Thus Ie =d lk [Ik kj + kj] ij(28) k whence I (29) so ii Ii I1 P'P' iij+ j Thislast jthat equation in the limit when the molecular magnetic moment is zeroj This lastequation states that in the limit whed the by cular magnetic moment is zero, the case of "perfect slip" which is approached by the large number of inner shell -11- _____11111__(1_11__-- __I· electrons in molecules made up of heavy nuclei, the effect of electronic interaction is to change the rotational energy from that calculated using nuclear masses to that using atomic masses, the method generally used. Exact correction for electronic interaction can be made from experimental magnetic moment measurements using Eq. 30. This entire derivation is of course based on the assumption Aij = Aji made in connection with Eq. 23; although it covers a very important class of molecules, molecules of very low symmetry are excluded. Generalization appears feasible but more involved. The tensor Gij has at worst the same symmetry as the nuclear system. For H 2 C 2 0 and D 2 C 2 O, symmetry C 2 v, it is diagonal. An estimate of Gij for H 2 C 2 0 is Gaa = + 0. 48 e/2Mv, IGbb = Gcc < 0. 05 e/ZMv where M is the proton mass. Use of these A below the value that figures results in decreasing the H-H distance by 2. 45 x 10 results from using atomic masses, and introducing a correction of less than + 4 x 10 5 A in the C=C=O distance. F. Structure The equilibrium structure is to be calculated from the equilibrium moments of inertia. We do not know the equilibrium moments, so the structure has been calculated from the moments of inertia extrapolated to zero centrifugal distortion. The errors assigned are taken roughly equal to an estimate of the correction resulting from the harmonic force constants, calculated on the assumption of a simple harmonic oscillator. Unfortunately, the structure of ketene is such that the carbon nucleus is, for all feasible isotopic configurations, so close to the center of gravity of the molecule that its position (+ 0. 10 A) has no effect upon the rotational spectrum. three structural parameters can be deduced from this work. tance can be calculated from IA of HzC 2 0 and D 2 C 2 O. Consequently, only First, the H to axis dis- This gives values 0. 9399 A and 0. 9406 A respectively (uncertainties in extrapolation to zero centrifugal distortion amount to + 0. 0010A here). Solving the expressions for I B of H 2 CzO and D 2 C 2 0 simul- taneously gives the length of the C=C=O chain and the projection of the C-H bond length along the symmetry axis as 2. 4751A and 0. 5210A respectively. The first of these is to be compared to the electron diffraction result (7) of 2. 52 + 0. 04A. The inertia defect / in the expression I C = I A + I B + a here amounts to 5 percent and 3 percent of I A for Hz2 C0 and D 2 C 2 0 respectively, so that IC calculated from this structure is in error by something of the order of 0. 2 percent. The measured moments of HDC 2O were used as a check, with the result shown in Table III. These errors are well outside the experimental error; calculations show that the length of the C=C=O chain varies only 6 x 10-5A per Mc frequency change of the J = 0-1 line, and that the component of the C-H distance along the symmetry axis varies 5 x 10-4A per Mc/sec. In this work, Planck's constant times Avogadro's number is taken as 39. 9066 x 10- 4 cgs; the present fractional error in this value (19) of -4 1:2. 3 x 10 , is not the limiting error in the final result, but is of the same order as the electronic correction. The structure is shown in Fig. 5. -12- ___ III. A. Stark Effect and Absorption Intensities Stark Effect The electric dipole moments determined from the Stark effect of the J = 0-1 transition of each molecule in the ground state, and of H 2 CzO in excited vibrational states, are listed in Table II. The difference in dipole moment between different isotopic forms is nearly within the experimental error. Some of the vibrational states have dipole moments differing from that of the ground tantp hv mn-rp Fig. 5 than the PYnPrimpntal estimated limits. Equilibrium structure of ketene from microwave data. Frrrv p-rr--r arp Agreement with the more impurity- sensitive method of Hannay and Smyth (9), which yielded 1.45 debye units, seems good. In general, the Stark effect is quadratic. Because the molecule is nearly symmetric, however, R branch transitions with K 1 = 1 have a quadratic Stark at low fields which changes to linear at high fields. K_1 > B. Intensities in the Ground Vibrational State R branch lines with 2 have essentially a linear Stark. The line breadth parameter was measured on the J = 0- 1 line of HC O 2 + 2. 0 Mc/mm. as 19. 8 Line intensities were then calculated from the Van Vleck-Weisskopf formula, with results consistent with rough estimates of intensity relative to nearby ammonia lines. In particular, the intensity alternation associated with the identical hydrogen nuclei in H 2 C 2 O and D 2 C 2 O was observed. The specific effect of this nuclear identity on transitions between levels in the ground vibrational state for HC O 2 is the increase of transition intensities between levels of odd K_ 1 by a factor of three. sities are increased by the same. factor for even K_ in accessible vibrational states. For D 2 CO, 2 1 Inten- values in transitions between levels ground vibrational state intensities for even K_ 1 are increased by a factor of two; again, transition intensities in accessible excited vibrational states have the opposite dependence on the parity of K 1. These facts further substantiate the C 2 v symmetry of the molecule. 3 have intensities of Lines with K = 3 are weak. H 2 C 2 O lines in K band with K_ -9 -7 cm -1 inapure 10 cm . D 2 C 2 O lines in K band with K 1 = 3 are about 1. 1 x 10 sample, and so could be detected, but K_ 1 = 4 lines are 7 x 10 cm 1 . No K_ 1 = 3 lines were searched for, however. Cooling the waveguide to dry ice temperatures is calculated to give an increase in line strength of a factor of about 4 for low-lying transitions. The vapor pressure of ketene at dry ice temperature was measured as roughly 200 mm of mercury. Intensities recorded in Table I for H 2 C 2 O and D 2 C 2 0 are calculated on the basis of a pure sample, but for DHC 2 O, on the basis of a 50 percent pure sample, which is the -13- ___X _I_ ___ _ _I _ I _ _ _ _ _ I maximum easily obtainable. C. Intensities in Excited Vibrational States For HC 2 0, the intensity ratio of the ground-state line to the vibration satellites corresponding to vibration fundamentals v 9 , v 8 and v 7 is 1:3 exp ( 3 exp (- . - -: 3 exp This involves the highly reasonable assumption that the lowest three modes of vibration are antisymmetric or "B" type. Thus, the intensity measurements already described imply the vibrational fundamentals listed in Table IV. The errors assigned are calculated from the estimated error of the intensity measurement (at room temperature, the frequency error in cm- 1 is twice the percent error in the intensity). Figure 6 shows the actual pattern of the J = 0-1 transition of H 2 C 2 0. The solid line connects our measured values, and limits of error assigned to these values are also Intensity points calculated from the vibrational fundamental assignments of Halverson and Williams (3) have also been plotted and connected by a dashed line. Barshown. ring an accidental and very unlikely coincidence of the satellites from vibrations v 6 and V7 , there is a definite disagreement for v 7. Although calculation of vibrational funda- mentals from rotational relative intensity measurement gives far less accuracy than the usual infrared techniques, the former method has the great advantage of freedom from the confusion of combination bands near the same frequency. The infrared spectrum of ketene has a large number of these which might result in difficulty of assignment of some of the fundamentals. 175 x 18 150 125 TE iE 100 (/ 75 z z 50 25 0 20,000+0 +10 +40 +20 +30 FREQUENCY - Mc Fig. 6 J = 0-J = 1 pattern of -14- +50 +60 pattern 1 of 1 6 C 2o +70 C) u In '0 C) 0 I o I I I ;> >> > > I I o I I N i I I o + 'O i I I + + I I NN N . o + . - o + 0 - L) 0 0 C I 0 0 C + a a .2C) 'a .C) ·7C)CC Q 0 0 II a' l II c . r- l" II IIII 0 0 0'Nr ' a, II >c II > I I i ' C)O) rn _ o C o rO l c o, . I l I I I ,I ,I :I . I aI I a I I a, L In u) 0 ) 'Q ac) I-' 0 u N - IL so r r- A 5auao '0 >, Sz 'd u0 a C) 0 0 X CO '0 N '0 '0 o X '0 o0 X 0 XC _ LA , o '0 r C o 0o X X o o Co 0- X 0 N CI 00 r o C5 o o c x x x x N '0 0'- N LA N cC$ Z rF C IC H -N -C) ao acl co co N N o o i co N o! i N X C)U I aI L l I I tN C) L · X '0 N eC ~;cr Nc ,.4 X X U oI N N N a' O) a, LI) 0 IC CCC a'+1 ! VaC 0r C) fN u: tN t N t - r a a) C) C t 00 o 'o N O '0 a, N '0 a' Ln a' - - .s t N r t t o a, cc _ N a' _ C No 9 N_ 9 N_ NN N 9 Ce N _ F Q r C) 0' 0 31 N '0 N '0 '0 0 '0 Nt a' N 0 t t t C) t _ _ _ t gN,s _ o N _ n t t __ _ N N .s.s U a,r.e a N t co o C) o o o o C o o C _ o , _ , f t t tN t _ N ,'0 _ _ N _ 0' o C 0 -15- _I_ t 0 _1C _Q IY__I_^·_ · SI-ll·-- - C) C) CC C) C) C) 0 C) C) I 0 o0 O 0 + + I C I I I I I I I I o O - C O O _ 0 C O 0 +0 C O O O 0 w ill C C . ) 0 :C OC) II II I 00 0 C 0 0 .-cC In a o U C) 0 to I° '0 0' L o r. au h. C) N I 0 C)" o o x x . _ o E- ) C) C 0 a C: O _ 0 _ N C~ C) L U N cN H 0 '0 rN w NCo O r LA o v 'o LA rCo) In~o S '0 N 0 N o C u - Q I 0 U 0 I -2*, C~ ) C 0 x 00 x > . ~ LA 00 L O LA 0 0 oo o 0 C 0 _: C O X a a,X~~~~~C o X . o Qo 0, C) C)u 0 0 Co 0 0 In N m a) 0' N C) ,9 rli Co 0' m C.) '0 0' '0 O 0 ',. oO a o N _ Ij 0' fn 11, 41 RC (o c 0 C)C CU) C) CC 0k C) C) N :C LA o , , N N CoO Cn N Co 0' - r c ,, N C) a)0 Co C .. Co _ _ ^ Co _, Nr ,. z, 0 ) LA r_ ^ 0 .N Pr C, ox w C) C) Sn 0 Caf U) CCe _ N N t -1 - t - _ _ C t t - NU _ _ N _ N Co N N C) - - - t t D t t N N '0 C o 0 o 0o 0' - t t 0' tO rq _ >1 0 t 0 o0 0 N rl _4 I I -16- __ I I '0t rsN rq f9 0'o t .s .9 N - U U C u] Q) N . U rO I I N N 0 0 E + o 0 I 0 ._0 U U I I , i '0 o I , I I 0 0 o 0 o o 0 0 + + _ o C o N o _ o o 0 0 0 0 0 m '0 ) ' It N N C0 N I ot 0 I a 11C' II 0 II >5 o c O O 0 I C- 0 0 0 0 a' *n L L a Cd o o oD o CCC U) o o I oI 1. I O I I 054 ddr 't w r- ri N m oor o · a o N ) Ien x v * C. VIU - N a,- .00 '0 I 0 o C.) o x X x X 'do N - V N 00 o C0 0o x X '0 FZ C u~~~~~a xX 0 oD co r- 0 o - o > > r- r- r o o 0 0 o N L C x x x X - 4 LA '0 I o _ x LA L X X X r - O or~ CC) c) 9xo 0 U 0 0In '0 n I LA I lo C'0 I I - I LA a'I _ C- c o oo0 o tcc I L, O 0 L c - o ,0 N - cc a' Ln CD N , 0'2 r- + n I U Uh _ X _ X _ X oo _ O O O U) n O n t U)c -N 't 0 oe * N C) C 0 '0 e o N LA In U, Cv '0 a' ¢- EC) C 0' C) , -~ ' N ' O N In L0 LA LA -t 'A '0 0 o _ t r o as o o or so N 0 U) N C t o o 0 N o t t o o o o o 0 N _ N N 0 N t _ 0 ctta t t t t t a _) -17- ___ N I-_ll·IIY··llli---YL··CIIIII - .1·111111111-1-1---_111- 1 N N A N 'i'' N O I +l 0o0 n o - -' Xa o 0 I I I I O .I 9+Io -+ I I 0, o I X I °o. a oo o + I 4 I I I _ e * + I I I 0 a ' +_ O + o '4-. 0 Id +1 + +I '+1 , I +1 ~~ O N d~ !" . ¢0 E- +01I +I '- 0" ' a I I I a I I a I a i a I a I I I I I I a a a N I i I 4 I 4I I 4I I a I III a I IN U. 4 i II. I I I g I C'- 4 4I 4 4 I a a I I a I I I I I 1 I I I I~~~~~~ I I I . I I LA a Ia 4 LA I a a I I I I I 4 4 I I I I I I I I I I I + I I IIt I i I I I I I 4 I I i I I I I I I 4 I I I I I I I I I I I I I I I I I I I I I I I I I I I I a) 0 a) a) I 4 a '. I . a a I I I 4 I I I '4 4 I I I a I § a I 0 4 I I a I II 4 . I I I I I U I aI I I I I a I I I ' I O a I I I ( I I I I a I I I I I I I 4 a a 4 I i I I I a I a i a I 4 4 I I 4. I 1 I I a I I I j g a I I I I I I II I I I I I I, g , I I I I I I I I I I I I I 4 I I I I I 4 4 I 4 4 I I I I I I I , , II I I Ln In Ln I I I 4 4 I I I a a 4 I I a 0 0+1 +1 0 0 Ln - +1 0 - I I N a I II a a II I I I I I 4 a I I I I a II I , I I 4 I o In N I I I f I vd 0 a) U0 0 In ooo> o 0 Cc ° o 0" N N 0X LA N + c°l I 5 '-,°, + + 0 a ! L - o _ O n. ' U2 H N I _ L II '~ (A) O e 0 +1 +1 ' 0 m '4" cw a'.0 .0 O o 0 +1 o _a _4 - 0 - a LA _ 5D +1 en - N 4- 4- c +I c +1 C N 4I 4C 4 N a - -18- - - d o 0 0 +1 0 - 0 L +1 O 4 I I I I I I I I I I I II C) d o 0 + C. + +I 0 o II II'-4 ii N) 4- I +1 0 g n'-' 0 ' Q) 4: I I I I 0 * ° 5 +1 +1 +1 c00o ° 00 o ¢S I 00 0 ' n n +1 '4' +1 ..a'4 0a'LA . O 0 o 00 F+O o dlC+1+1 ( ~N t' - req 0o N' . = o 0 +1 0 Lr 0 Table III Moments of Inertia of HDC20, AMU-A 2 Calculated IA 2 Measured 2. 5946 Error 2.5914 0.12 percent IB 52. 320 52. 377 0.03 percent IC 54.972 55.089 0.21 percent Table IV Comparison of Microwave and Infrared Measurements of Vibration Frequencies, cm 1 V9 Microwave IV. V8 565 + 20 487 + 15 V7 v6 674 + 30 Halverson and Williams 529 588 909 1011 Drayton and Thompson 540 600 910 995 Conclusion A more accurate structure evaluation for ketene depends mainly upon correct cal- culation or measurement of the zero-point vibration interaction. It appears that this would be difficult at present. Further measurement of the spectrum of D 2 C 2 0 would be extremely interesting as a more complete check on centrifugal distortion theory applied to a molecule with both Q and R branch transitions; besides investigating how well the rotational spectrum can be fitted to the theory,*actual calculation of the coefficients from the vibrational fundamentals would be feasible for ketene because of its symmetry. R branch sets measurable are J = 0-l1*, 1-2*, 2-3, 3-*4 and 4-5; Q branch series measurable have K = 1*, 2* and 3. Those starred have actually been measured. Possibly, further work on the vibrational spectrum is also indicated. -19- -.----. --- ---- Referenc es 1. H. A. Wooster, C. C. Lushbaugh, C. E. Redeman: 68, 2743, 1946 Toxicity. 2. H. Gershinowitz, E. B. Wilson, Jr.: Infrared. Chem. Phys. 5, 500L, 1937 3. H. Halverson, V. Z. Williams: Infrared. J. Chem. Phys. 15, 552, 1948 4. W. R. Harp, R. S. Rasmussen: J. Chem. Phys. 15, 778, 1948 5. L. G. Drayton, H. W. Thompson: Infrared. 6. H. Kopper: Raman, Liquid. 7. J. Y. Beach, D. P. Stevenson: Electron Diffraction. 8. G. Forster, R. Skrabal, J. Wagner: 9. 10. 11. Infrared. J. J. Am. Chem. Soc. J. Chem. Soc. 1416, 1948 Z. Phys. Chem. B34, 396, 1937 J. Chem. Phys. 6, 75, 1938 Ultraviolet. Z. Elektrochem. 43, 290, 1937 N. B. Hannay, C. P. Smyth: Dipole Moment. J. Am. Chem. Soc. 68, 1357, 1946; Comment on 9. A. D. Walsh: J. Am. Chem. Soc. 68, 2408L, 1946B. Bak, E. S. Knudsen, E. Madsen, J. Rastrup-Anderson: Microwave. Phys. Rev. 79, 190L, 1950 H. R. Johnson, J. G. Ingersoll, M. W. P. Strandberg, J. Goldstein: Microwave. Bull. Am. Phys. Soc. 26, No. 1, 40, 1951 12. R. B. Lawrance, M. W. P. Strandberg: Centrifugal Distortion. Technical Report No. 177, Research Laboratory of Electronics, M.I.T. October 1950 13. R. E. Hillger, M. W. P. Strandberg: Centrifugal Distortion. Technical Report No. 180, Research Laboratory of Electronics, M. I. T. (to be published) 14. J. W. Williams, C. D. Hurd: Manufacture. 15. M. T. Weiss, M. W. P. Strandberg, R. B. Lawrance, System. Phys. Rev. 78, 202, 1950 16. H. H. Nielsen: Vibration-Rotation Interaction. 540, 1942 17. G. W. King, R. M. Hainer, P. C. Cross: Asymmetric Rotor Theory. Phys. 11, 27, 1943 18. J. R. Eshbach, M. W. P. Strandberg: Molecular Magnetic Moment. Technical Report No. 189, Research Laboratory of Electronics, M. I. T. (to be published) J. W. M. DuMond, E. R. Cohen: Values of Constants. Rev. Mod. Phys. 20, 82, 1948 19. 20. G. C. Wick: Magnetic Moment Estimation., J. Org. Chem. 5, 122, 1940 C. C. Loomis: Stark Phys. Rev. 60, 794, 1941, 61, J. Chem. Phys. Rev. 73, 51, 1948 Acknowledgment The authors are grateful to R. C. Lord of M. I. T., who supplied the deuterated acetone, to J. G. Ingersoll, who participated in most of the experimental work, to B. V. Gokhale for many profitable discussions, and to J. Goldstein of Harvard for his cooperation in the initial phases of this work. Ryder assisted in the numerical computations. -20- _ Miss Mida Karakashian and Mrs. Neria