APPROACHES AND CHALLENGES FOR 3D IC PACKAGING Charles G. Woychik, Sangil Lee, Guilian Gao, Liang Wang, Hong Shen, Akash Agrawal, Mohamed Elassar, Scott McGrath and Sitaram Arkalgud Invensas Corporation 3025 Orchard Parkway San Jose, CA USA Cwoychik@Invensas.com ABSTRACT Recent product announcements highlight the emergence of higher volume TSV-based products in the marketplace. Major industrial players have launched products leveraging TSV technology such as the DDR4 3D stacked DIMM, high bandwidth memory (HBM), and high performance graphic processors using a 2.5D Si-interposer. While offering considerable performance, power and density advantages, packaging costs still remain high and need to be reduced further. This paper presents a detailed study and data on assembling a 2.5D test vehicle. The test vehicle used consisted of two 10mm x 12 mm micro-bumped die having solder capped Cu-pillars with a 60um pitch attached to a 19mm x 27mm Si-interposer with a thickness of 100um and TSVs having a dimension of 10um x 100um. This Siassembly was then attached to a standard buildup substrate. A discussion of the challenges for thermal compression bonding thin die to an interposer and the impact of subsequent flip chip attach reflow of the Si-assembly to the interposer on the integrity of the micro-bumped die interconnects is discussed. Once the optimized bonding conditions were achieved, samples were built and subjected to MSL L3 preconditioning and thermal shock testing (TST). The assembly challenges and the resulting reliability tests results will be discussed in this paper. Key words: 2.5D, 3D IC, TSV, Micro-bumped die, Siinterposer, CTE, warpage, JEDEC reliability specifications, chip stacking. INTRODUCTION Very high end 3D packaging uses through silicon vias (TSVs) to produce a three dimensional stacked semiconductor chip structure. The ability to create a three dimensional heterogeneous integrated semiconductor structure offers numerous benefits, such as power reduction, performance improvement and miniaturization. The viability of the semiconductor technology to create these TSVs in volume has been demonstrated. However, making this a cost effective technology is where the focus needs to be in order to make this viable for high volume manufacturing [1-3]. The recently announced 2.5D AMD Radeon R9 Fury module shows the integration of a 3D memory stack along with a large die GPU on a Si-interposer as shown in Figure 1. Prior to this announcement the Xilinx Virtex 7 2.5D Siinterposer product was the one most often cited at conferences and in publications. The Virtex 7 has four planar rectangular die attached to a Si-interposer and has a very high ASP. In comparison, the AMD product is a more sophisticated design since it uses 4 HBM 3D memory stack modules with TSVs along with a large die GPU, all of which are attached to a Si-interposer. It was also dramatically cheaper than the Xilinx offering. The cost of making TSVs and 3D stacking is coming down dramatically. To enable wide adoption of 2.5D and 3D technology, an important question must be answered: Who will do the 3D IC assembly? In the past, the semiconductor fabricator (IDM) designed and manufactured the die and then handed it over to the packaging facility for assembly and test. As flip chip technology evolved, a new sector called the “middle end” developed which included RDL, wafer bumping and test. This middle region has further evolved to include micro-bumping, wafer thinning and backside reveal, interposer fabrication, wafer level assembly and 3D wafer level test. As the industry develops this technology, we realize that the packaging solution for the foundry is likely to be different from that of the OSAT. The turnkey chip-onwafer-on substrate assembly flow suits a foundry model very well but does not involve an OSAT. Alternative assembly flows that use chip-to-interposer-to-substrate approach are much more OSAT inclusive. In this paper we focus on an OSAT type of assembly method that can offer a high yielding, and therefore lower cost, 3D packaging solution. (a) Figure 1. Photo of AMD’s large die GPU and 4 Hynix HBM modules attached to a Si-interposer (Image courtesy of AMD). In developing a package solution, one must engineer this package to be able to pass the JEDEC standard module and board level reliability tests, which are temperature cycling, high temperature storage, temperature and humidity testing, unbiased high accelerated stress testing (HAST), and pressure cooker testing. Based on our experience in developing reliable packages, we know that understanding stress and its impact through the assembly process can have a dramatic effect on the final warpage of the assembled package. This warpage will affect the final reliability of the package, which is why it is paramount to properly engineer the package & assembly process in order to minimize the ITP and substrate warpage. Much research has been done to investigate the effect of warpage on reliability of organic flip chip packages and substrates, and this knowledge can be applied to current 3D IC packaging designs [4-7]. (b) Figure 2. A schematic illustration of the 2.5D test vehicle having two micro-bumped die attached to a Si-interposer, which is then attached to a buildup substrate. (a) overall test vehicle; (b) partial X-sectional corner view showing the part with underfill and mold cap. TEST VEHICLE DESIGN The 2.5D test vehicle used in this study is schematically illustrated in Figure 2. Two micro-bumped die (MBD) are attached to a Si-interposer (ITP), which is then attached to a standard buildup substrate. Details of the test vehicle design are given in Table 1. In this test vehicle, the ITP dimensions are 19.25mm x 27.05mm x0.1mm. The buildup substrate has a 3-4-3 layer structure. On the top surface of the ITP are two MBD with dimensions of 10mm x 12mm and a thickness of 0.2mm. The two MBDs were spaced 2mm apart. Table 1. The Invensas 2.5D test vehicle specification FABRICATION OF Si-INTERPOSER (ITP) AND MICRO-BUMPED DIE (MBD) The ITP was made on 300mm wafers using a via-mid process. The TSVs had a 10um diameter and were 100um deep. A standard DRIE dry etch process was used to form via holes in the wafer. A standard PECVD TEOS process was used to deposit the SiO2 isolation layer. A Ta-Cu barrier/seed layer was deposited and the vias were filled using a Cu-electroplating process. There was one RDL layer on the front side and one layer on the backside. Front side passivation was silicon oxide. The backside passivation was a combination of low temperature silicon oxide and low temperature cured polyimide. Figure 3 shows a SEM crosssection image of the interposer with pads for microbump attachment on the top and UBM for flip chip ball on the bottom. (a) (b) Figure 4. (a) An SEM image of the reflowed, solder capped microbumps on a MBD; (b) SEM image of a pillar with Cu base and solder cap. Figure 3. SEM image of a cross-section of the Si-interposer used for this study. The MBD was also made on a 300mm wafer. The surface was passivated with silicon oxide. One copper RDL layer was used for daisy chain connection between the microbumps. The 35um diameter Cu pillars with SnAg solder cap were produced by electroplating. The solder cap was reflowed to form the half-dome shape after the plating resist was stripped. Figure 4 shows SEM images of the solder capped Cu-pillar bumps on the MBD. ASSEMBLY PROCESS FLOW Different assembly flows including fab centric and OSAT centric flows were evaluated at Invensas. In this paper, we concentrate on the OSAT friendly, substrate-last assembly flow shown in Figure 5. For this assembly flow, a singulated ITP, either with or without backside solder bumps was held in place with a vacuum fixture. This study used an ITP having ENIG pads on the topside for MBD attach, as shown in Figure 4. The two MBD were then attached to the ITP with in-situ solder reflow using a thermal compression bonder and then underfilled. The assembled ITP was attached to the substrate using a conventional mass solder reflow process. In this study the solder balls were placed on the substrate, and then the substrate was attached to the ITP using mass reflow. As shown by Gao, et. al[8], this assembly flow minimizes the ITP warpage with vacuum during the MBD attachment. Consequently it can meet the very narrow assembly window of 11um for the MBD attachment. More details on these process flows are outlined in a recent publication [9]. The focus of this paper will be the process assembly development related to process conditions and materials selection. Figure 6. X-ray image showing microbump solder bridging in the perimeter array after assembly to the ITP. Figure 5. Substrate-last process flow using a solder bumped interposer with a non-solder bumped substrate (left side) and a non-solder bumped interposer in combination with a solder bumped substrate (right side). Solder capped copper pillar micro bumps were used to attach the MBD to the ITP. The perimeter array is 60um pitch and the inner array is 120um pitch. The ITP was attached to the 3-4-3 buildup substrate with 110um diameter solder balls. The perimeter array was 180um perimeter pitch and the inner array was 250um pitch. Solder balls were attached to the substrate prior to die assembly. Both the MBD and the ITP are underfilled using commercially available capillary underfill materials. There are two units on each substrate strip. Following underfill cure, the entire strip is molded with a transfer mold process using a Invensas qualified HVM mold material. ASSEMBLY PROCESS DEVELOPMENT In this work, design of experiments (DOEs) were used to achieve a high yielding MBD to the Si-ITP attachment process. When the initial set of parts were built, the primary failure mode was microbump solder bridging. Figure 6 shows an X-ray image of these bridges in the 60um pitch periphery array of the microbumps after assembly to the ITP. To achieve the final process window, three different DOEs, two for the MBD to ITP attachment process by TCB, and one for flux selection, were designed and carried out. The first DOE focused on optimization of thermal and mechanical process parameters affecting solder bridging of the microbumps. The second DOE validated the stability of the assembly process. The third DOE studied the effect of two different fluxes on microbump joint integrity DOE1: TCB PROCESS OPTIMIZATION The primary objective of DOE1 was to decouple thermal and mechanical process parameters in MBD attach using a TCB bonder. Thermal process parameters included bond stage temperature, bond head peak temperature, time at peak temperature and vacuum release temperature during cool down. During bonding one must account for the collapse of the solder capped Cu-pillar due to the melting of the solder. In order to prevent total collapse, the TCB bonder used in this study has a z-displacement setting to control the amount of z-displacement of the head. This amount of controlled zdisplacement after solder reflow is called the “Melt Setting.” Task 1 used a fixed melt setting to identify a stable thermal process window. Then Task 2 optimized the mechanical parameters, i.e, the melt setting, within the optimized thermal process conditions. Task 1- Thermal Process Parameters Evaluation: In this task, the three variables were evaluated: bond stage temperature, time at peak temperature of the bonding head, and vacuum release temperature during cool down. The peak temperature of the bonding head was set at 305C. The melt setting use was 6um. This experiments produced the nominal MBD interconnect height of 43.2 um. The target height that we wanted to achieve was 35um, which was based on assembly window analysis [8]. Figure 7 shows a SEM of the resulting solder interconnect from this build. Under these conditions, the failure mode has shifted from solder bridging to solder opens. For all four legs of the DOE there were solder opens as shown in Table 2, which implies that the thermal process window is stable enough not to result in short failures and mechanical process window is independent of thermal process parameters because no short failures were observed at even higher temperature and longer peak. Solder wetting 6um 8um 10um Figure 7. The nominal MBD solder interconnect height of 43.2um from DOE1 Task1. --- Melting Setting Figure 8. DOE1 Task 2-TCB profile Parts built using these process parameters were crosssectioned for stand-off height evaluations. The result shows a slight bow of the die with the stand-off height in the center approximately 2um taller. We believe that this bow was due to a temperature gradient across the MBD that causes an uneven gap height. Figure 9 shows the edge MBD solder joints having a height of 40um and the center die solder joints having a height of 42um. Table 2. DOE1 Task1–Thermal process parameters and results Task2: Mechanical Process Parameters and TCB Process Design: In Task 2, we selected upper limits of the thermal process window identified in Task 1, which do not induce short failures, to guarantee stable solder interconnection. The mechanical process condition, i.e, the melt setting was then adjusted to eliminate solder opens. As shown in Table 3, melt settings of 6um, 8um and 10um were evaluated. 40um ~40um m Edge 42um ~42um Center Figure 9. Comparison of edge and center MBD interconnect height using DOE1 bonding conditions. Table 3. Melt settings with thermal process conditions used in DOE1 Task 2 From this work the electrical testing of the daisy chain test structure confirmed no solder opens and no shorts when using a melt setting of 10um. Electrical testing and X-ray was also used to verify no short failures. The thermal bonder conditions used for this build are shown in Figure 8, which shows the locations for the 6um, 8um and 10um melt setting conditions. Also, it was found that the intermetallic compound (IMC) thicknesses varied on the MBD interconnect. Figure 10 shows a 2.1- 2.8um IMC thickness range at the solder to Cu pillar interface whereas only a 1.2um IMC thickness at the solder to ITP pad interface. This can be explained by the fact that the solder capped Cu-pillar saw two reflows whereas the ITP pad saw just one solder reflow. The amount of IMC on the die side prior to assembly was approximately 1um. 300C Head Twice reflowed (1.Solder Target: <3um One reflow time reflow 130C Stage Figure 10. IMC thickness variation on the top and bottom of the MBD interconnection. As mentioned previously, the goal was to develop a process having a MBD interconnect nominal height of around 35um and having no solder bridges or opens. Figure 11 shows the details of DOE2. Stage Temp 150C Hold time 1sec Future Process Window Investigation 140C 130C 3sec Current Process Window Melt setting 6um 8um 10um 5sec 12um DOE2: TCB BONDING PROCESS WINDOW VALIDATION In order to validate the best process window conditions derived from DOE1, a set of 36 interposers were assembled using the process conditions shown in Table 4. From this build 33/36 parts passed electrical test with no solder defects. Bonding Conditions: • • Gap Control = -10um Flux Type/Dip = ABC / 5um • Force = 2.8N • • • • Stage Temp = 130C Contact Temp = 130C Peak Temp/Time = 305C / 5sec Release Temp = 130C 91.7% MBD Yield: 33/36 MBD Passed e-test “Good” ITP Table 4. Build conditions to validate DOE2 process window. Moreover, after careful failure analysis of the 3 parts showing electrical test open failures, it was determined that all three were due to opens in the RDL trace in the MBD daisy chain. Figure 13 shows an SEM image of the open in the trace on the MBD side. When this open defect was compared with a good interconnect, it was found that the good interconnect had no metallization defects, explaining why these 3 assemblies failed. Figure 11. DOE2–Process window definition A melt setting of 12um resulted in solder bridging. Only a melt setting of 10um yielded a nominal joint height of about 32um without any opens or bridges. Figure 12 shows a comparison of the nominal MBD interconnect heights when a melt setting of 6um and 10um was used. For the 6um melt setting a nominal joint height of 42.6um was achieved, and for a 10um melt setting a nominal joint height of 31.8um was achieved. Melt Setting 6um 42.6um Open Unit Melt Setting 10um 31.8um Figure 12. Comparison of MBD nominal joint heights, melt settings of 6um and 10um using DOE2. Figure 13. SEM image showing open defect in the trace. DOE3: Impact of Flux on MBD Integrity Some parts built with flux A that passed electrical test after MBD attach and underfill showed electrical failure after the ITP- to-substrate assembly process. Cross-section and SEM examination of the failed parts showed non-setting at the solder to ITP bonding pad interface (Figure 14). Weak flux activity was suspected to be the root cause of the failure. In DOE3, we evaluated the effect of two different flux materials, Flux A and Flux B, on interconnect integrity. Flux B has higher activity and also leaves very low residue. MBD to the ITP joint after the ITP had been assembled to the substrate through a conventional solder reflow process. Table 5 shows the bonding conditions used for DOE3, which were the optimized conditions from DOE1 and DOE2. Three different flip chip reflow profiles were investigated: 130s, 90s and 60s as time above liquidus (TAL). In the conditions using Flux A, only the parts using 130s TAL showed complete MBD integrity. Both the 90s and 60s TAL showed failures in the MBD solder interconnect. Figure 15. SEM image showing good MBD integrity after bonding using Flux B All parts built using Flux B showed good MBD joint integrity after post flip chip reflow and cleaning. Figure 15 shows an intact MBD interconnect using Flux B. This image was representative of all three TAL conditions. Therefore Flux B was chosen as the POR material for the TCB bonding. Figure 16 shows a representative CSAM image of the underfilled MBD in which there are no voids after curing the underfill material Figure 14. SEM image of a part build using flux A showing non-wetting at the solder to ITP pad interface. Stage Temp (C) Contact Temp(C) Peak Temp Release Temp(C) Contact Force(N) Melt Setting (um) 130 130 305C for 5sec 130 2.8 10 Table 5. Optimal MBD bonding conditions used for DOE3 Figure 16. CSAM image of MBD after assembly using Flux B, 90s TAL. Table 6 shows summary of DOE3 results. From this testing one can see that the POR flux material passed all three TAL conditions. In addition the parts built with Flux B were subjected to an additional TST for 200 cycles and did not show after failure. Table 6. DOE3 Results Summary of the results 16 parts built using Flux B (POR) were subjected to MSL Level 3 pre-conditioning and 3X solder reflow per JEDEC standard. All 16 units tested passed MSL Level 3 test. The parts were further subjected to 200 cycles of thermal shock from -55C to 125C. All 16 units passed the test. DISCUSSION The main focus of this assembly process development was to establish an assembly process window that was compatible with OSAT assembly facility. In this approach a Si-to-Si bonding of the solder capped Cu-pillars on the MBD was done to a non-bumped Si-ITP using thermal compression bonding. The challenge was to create the right process conditions that can produce a high yield with no solder bridges or opens. As can be seen from the experimental flow, first we experienced solder bridging. Once the solder bridging was eliminated using the conditions of DOE1 Task 1, the next goal was to eliminate the solder opens, which was the objective of Task 2. From Task 2, solder opens were eliminated, however, the nominal solder interconnect height was about 43um, which was higher than the target of 35um. In DOE1 Task 2, the melt setting was varied and it was determined that a value of 10um produced no solder opens. This was based on bonding 70 die in which we achieved a 90% assembly yield, in which the remaining 10% failures were due to cracked traces on the micro bumped die (as shown in Figure 13). Also, from this work, we were able to plot the gap height versus melt setting and determine the best condition to achieve a nominal interconnect height of 35um. Figure 17 shows a linear regression plot of the gap height versus melting setting from this particular build. These are single measurement points made at the same location, which is the center of the micro bumped die. are very confident in achieving a process window that can produce a high yield MBD to Si-ITP assembly yield. CONCLUSIONS 1. A 2.5D assembly process using a substrate-last assembly flow has been developed at Invensas and demonstrate high assembly yield for MBD to SiITP attachment 2. Proper flux selection was critical for the microbump solder joint integrity and moisture reliability. 3. The process flow is OSAT friendly and can enable leverage of existing manufacturing infrastructure at the OSAT to meet high volume demand for future 2.5D and 3D assembly. . ACKNOWLEDGEMENTS The authors would like to acknowledge the help and support of the engineering team at the company. Special thanks are extended to Bong-Sub Lee, KM Bang, Grant Villavicencio, Hala Shaba, Roseann Alatorre and Gabe Guevara for their engineering work in design, assembly and characterization. REFERENCES 1. B. 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