Revision T February 2007 SPACE SHUTTLE MISSIONS SUMMARY Page 158 - STS-107 LANDING SSME-TL CREW LAUNCH SITE, SITE/ NOM- SRB ORBIT PAYLOAD MISSION HIGHLIGHTS (7) FLT ORBITER LIFTOFF RUNWAY, ABORT RSRM FSW WEIGHTS, (LAUNCH SCRUBS/DELAYS, TIME, CROSSRANGE EMERG NO. LANDING LANDING THROTTLE AND INC HA/HP PAYLOADS/ TAL WEATHER, ASCENT I-LOADS, TITLE, NAMES SITES, TIMES PROFILE ET EXPERIMENT FIRSTS, SIGNIFICANT ANOMALIES, ETC.) & EVA'S ABORT TIMES FLT ENG. S.N. S DURATION, WINDS Revision T February 2007 SPACE SHUTTLE MISSIONS SUMMARY Page 258 - STS-107 STS- OV-102 CDR: KSC 39A 104/104/ BI-116 39. DIRECT OI- CARGO: KSC W/D: OPF 79, VAB 9, PAD 35 = 123 days 107 (Flight 28) Rick D. Husband 16:15:39:00Z 109% 0 INSERTION 29 35463 LBS total. (Flt 2 - STS-96) 10:39:00 AM RSRM (8) (5) LAUNCH POSTPONEMENTS: SEQ Columbia EST (P) PREDICTED: 88 POST OMS- PAYLOAD - Baselined launch date of 1/11/01 on 11/10/99. FLT #113 P690/R248/V177/M21 10:39:00 AM 100/104.5/7 2: CHARGEABLE: - Postponed launch date to 2/22/01 on 3/3/00. OMS 6 EST (A) 2/ ET-93 156 x 147 24316 LBS - Postponed launch date to 4/15/01, then KSC-113 PODS: Thursday 34 72/104.5 NM 6/14/01, others(?), then to 9/2/03, moved after LPO5-17 PLT: 1/16/03 (10) DEORBIT LWT-86 DEPLOYED: STS-112 and STS-113 (Priority flights to HST and RPO5-16 BURN: ACTUAL: 0 LBS ISS flights that had been postponed due to flow- PAD 39A- William C. McCool liner cracks.) 40 FRC2-28 P691/R290/M254 LAUNCH 32:13:15:18Z 100/104.5/7 WINDOW: Sunday, 2/ ET NON- - Postponed launch date to 1/16/03. MLP-1 EDO FLT M/S 1: 2H30M CTOB February 1, 72/104.5 IMPACT DEPLOYED: LAUNCH SCRUBS: None 15 David M. Brown 2003 23515 LBS S/H RDM 1 P692/R291/M255 EOM PLS: KSC 1 = 2055 (1) 1:24:35 LAUNCH WINDOW: TAL: MRN PLANNED 2 = 2053 (5) MET MIDDECK: - Launch Window was 2H30M (Crew Time On M/S 2: TAL WX: ZZA LANDING: 3 = 2049 (7) 801 LBS Back). Kalpana Chawla On KSC 33 at LAT: SELECTED: ° LAUNCH DELAYS: NONE (Flt 2 - STS-87) 9:15:50 AM 2.28 N SHUTTLE - KSC weather was excellent, perhaps the best RTLS: KSC 15 EST ACCUMULATE CI/N launch weather experienced in Shuttle Program. P693/R230/V178/F30 LONG: D - Launch occurred On-Time at 16:15:39:00Z, TAL: MRN 20 ORBIT 139.42° WEIGHTS: 10:39:00 AM EST, on Thursday, January 16, N/N M/S 3 (PAYLOAD DIRECTION: W DEPLOYED: 2003. AOA: EDW 04 DL 49 1189722 LBS CDR): CI/N TAL WX: Michael P. Anderson NON- PLS: EDW 04 DEPLOYED: - Moron was prime and selected. Both Moron (Flt 2 - STS-89) N/N and Zaragoza were forecast and observed GO. 1559554 LBS Ben Guerir was not available. CARGO TOTAL: P694/R235/V179/M20 TDEL: 3547208 LBS PERFORMANCE ENHANCEMENTS: 5 0.11 - Standard Set plus: PE Operational High Q 0.032/0.070 PERFORMANC (WIN/JAN) and OMS Assist. M/S 4: E MARGINS Laurel Blair Salton MAX Q NAV: FIRSTS/LASTS: (LBS): - First flight of Space Shuttle in CY 2003. Clark 756 749 FPR: 3047 P695/R292/F37 - First flight of Spacehab RDM (Research Double SRB STG: FUEL BIAS: Module) with more than 80 Experiments. 2:05.4 2:07 1112 Science: Biological, Physiological & P/S 1: FINAL TDDP: Countermeasures, Physical Sciences, Earth and Ilan Ramon RECON: Space Science, Space & Technology (ISRAEL) PERF: NOMINAL Development. P696/R293/M256 - First EDO Pallet Flight since STS-90 (April 17, 2 ENG TAL PAYLOADS: 1998) (MRN): PLB: - First flight of Israeli Astronaut - Ilan Ramon 2:39 2:50 SPACEHAB RDM FLIGHT DURATION CHANGES: NEG RETURN: FREESTAR - Planned landing at KSC on orbit 256 (TIG orbit 3:50 3:52 OARE 255) on Saturday, February 1, 2003. Deorbit EI: (MORE THAN maneuver was initiated at 32:13:15:18Z, 8:15:18 PTA (U/S 242): AM EST on Saturday, February 1, 2003 (TIG orbit 80 255, landing orbit 256). Planned landing time 5:15 5:14 WEIGHT: EXPERIMENTS) was 32:14:15:50Z, 9:15:50 AM EST. 234495 LBS - Orbiter weight and Xcg at entry interface was SE OPS 3: MIDDECK: 234,495 lbm, Xcg was 1078.53. 5:25 FLT DURATION: X CG: FREESTAR - - Orbiter weight and Xcg at entry interface plus 15:22:20:32 1078.53 DEORBIT: MIDDECK H/W 15 minutes 234,167 lbm, Xcg was 1077.87. PTM (U/S 242): Lost contact Ha 151.6 RAMBO - Flight controllers reported increased 5:54 6:05 temperatures on some sensors and some failed with Columbia NM S/H SUPPORT sensors in left wing area. Off-nominal SE TAL (ZZA): at 8:59:32 AM EI + 15 MIN: Hp 135.0 EQUIPMENT indications started at approximately 5:56 6:05 EST NM 32:13:52:17Z. Columbia contact loss (Loss-of- WEIGHT: Signal) occurred at 32:13:59:32Z, 8:59:32 AM S/T: 234167 LBS VELOCITY: 9 CRYO TK EST (15:22:20:32 MET), 16 minutes prior to MCC WHITE FCR (43) SE PTM (U/S planned landing time. Communications and 459): 1031:11:54:42 25762 FPS SETS X CG: (EDO PALLET) tracking were lost at an altitude of FLIGHT DIRECTORS: 7:00 7:05 approximately 203,000 feet while Columbia was OV-102: 1077.87 ENTRY traveling at approximately 12,500 miles per hour LD/O 2 - K. B. Beck 300:17:39:40 RANGE: 5 GN2 TANKS O 1 - J. S. Stich MECO CMD: at Mach 18. 8:20.9 8:23 4439 NM - Columbia and 7 astronauts were lost over O 3 - B. P. Austin DISTANCE: NO RMS Texas. O 4 - J. M. Hanley VI: 6,649,757 sm A/E - L. E. Cain 25863 25860 RED SHIFT: Rick Husband, Kalpana Chawla, MOD - P. L. Engelauf Laurel Clark, Ilan Ramon. OMS-2: 41.18 41:24 BLUE SHIFT: William McCool, David Brown, Michael Anderson (PL CDR) Revision T February 2007 SPACE SHUTTLE MISSIONS SUMMARY Page 358 - STS-107 Revision T February 2007 SPACE SHUTTLE MISSIONS SUMMARY Page 159 - STS-107 LANDING SSME-TL CREW LAUNCH SITE, SITE/ NOM- SRB ORBIT PAYLOAD MISSION HIGHLIGHTS (7) FLT ORBITER LIFTOFF RUNWAY, ABORT RSRM FSW WEIGHTS, (LAUNCH SCRUBS/DELAYS, TIME, CROSSRANGE EMERG NO. LANDING LANDING THROTTLE AND INC HA/HP PAYLOADS/ TAL WEATHER, ASCENT I-LOADS, TITLE, NAMES SITES, TIMES PROFILE ET EXPERIMENT FIRSTS, SIGNIFICANT ANOMALIES, ETC.) & EVA'S ABORT TIMES FLT ENG. S.N. S DURATION, WINDS Revision T February 2007 SPACE SHUTTLE MISSIONS SUMMARY Page 159 - STS-107 STS- Continued… 107 Continue STS-107 EVENTS: d… Orbital Altitude was 150 nm. STS-107 FLIGHT OBJECTIVES/EXPERIMENTS: - Flight was a dedicated and successful science/research mission. - Primary payload is SPACEHAB Research Double Module (SHRDM) with International, NASA and SPACEHAB commercial payloads including Life Sciences, Materials, and Microgravity Science Research Experiments. - Fast Reacting Experiments Enabling Science, Technology, Applications and Research (FREESTAR) is a complex Secondary Payload which is a cross bay carrier with following payloads: MEIDEX (Mediterranean Israeli Dust Experiment), Solar Constant-3 (SOLCON-3), Shuttle Ozone Limb Sounding Experiment-2 (SOLSE-2), Critical Viscosity of Xenon-2 (CVX-2), Low Power Transceiver (LPT), and Space Experiment Module-14 (SEM-14) - Ram Burn Observation (RAMBO) SIGNIFICANT ANOMALIES: - ET Foam loss during ascent at approximately 81 seconds (likely from Bi-pod area) (IFA). Re- design constraint to flight. - RSRM Nozzle Flex Boot Separation (IFA). Constraint to flight. - O2 Tank 7 Heater failed off in Manual Mode (IFA STS-107-V-02) - Suspected Fuel Cell Monitoring System Data Cable problem. FCMS is suspect after same problem with backup cable. - SM I/O Errors on IP Bus - DSR 20 Error Message 32 (Loss of tape recording and playback) - 70 mm Hasselblad Intermittent Motor Drive (Binds or jams) - 2nd 70 mm Hasselblad Motor Jam - STGT site outage - Payload No I-COM B Transmission in Spacehab (Not being heard in Spacehab) - Spacehab water loop Degradation (Flow rates decreasing) - Payload Ku Channel 2 Data Dropouts (Ku-Band and S-Band) - AC2 Phase B “Sluggish” Current Signature on Orbiter (IFA STS-107-V-01) - Forward DAP Auto A Contact Deselected by RM - Spacehab Rotary Separator flooding short - Loss of Columbia and crew during Entry - IFA STS-107-V-03 CAIB REPORT: Accident Analysis indicated that the physical cause of the loss of Columbia and its crew was a breach in the Thermal Protection System on the leading edge of the left wing. The breach was initiated by a piece of insulating foam that separated from the left bipod ramp area of the External Tank and struck the wing in the vicinity of the lower half of Reinforced Carbon-Carbon panel 8 at 81.9 seconds after launch. During re- entry, this breach in the Thermal Protection System allowed superheated air to penetrate the Revision T February 2007 SPACE SHUTTLE MISSIONS SUMMARY Page 159 - STS-107