Space Shuttle Missions Summary
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Revision S May 2002 SPACE SHUTTLE MISSIONS SUMMARY Page 111 - STS-95 CREW LANDING SITE/ SSME-TL (7) LAUNCH SITE, RUNWAY, NOM- SRB ORBIT PAYLOAD MISSION HIGHLIGHTS FLT ORBITER LIFTOFF TIME, CROSSRANGE ABORT RSRM FSW WEIGHTS, (LAUNCH SCRUBS/DELAYS, EMERG NO. TITLE, NAMES LANDING SITES, LANDING TIMES THROTTLE AND INC HA/HP PAYLOADS/ TAL WEATHER, ASCENT I-LOADS, & EVA'S ABORT TIMES FLT DURATION, PROFILE ET EXPERIMENTS FIRSTS, SIGNIFICANT ANOMALIES, ETC.) WINDS ENG. S.N. STS-95 OV-103 CDR: KSC 39B KSC 33 (KSC 45) 104.5/104.5/ BI-096 28.45° DIRECT OI-26B CARGO: KSC W / D : OPF 76, VAB 5, PAD 29 = 110 days (Flight 25) Curtis L. Brown 302:19:19:33:98Z 311:17:03:30Z 109% (47) INSERTION (3) 38618 LBS 2:00:00 PM EST (P) 12:03:30 PM EST LAUNCH POSTPONMENTS : SEQ FLT #92 Discovery (Flt 5 - STS-47, STS-66, RSRM 2:19:34 PM EST (A) PAYLOAD - Baselined launch date of 10/8/98 on 7/31/97. STS-77, STS-85) Thursday 28 Saturday 20 PREDICTED: 68 POST OMS -2 : OMS PODS : CHARGABLE: - Postponed launch date to 10/29/98 on 12/18/97. KSC-92 P539/R152/V112/M136 10/29/98 (10) 11/7/98 (11) 100/104.5/ 303 X 295 NM 28520 LBS LPO1 - 28 104.5/67/ ET-98 LAUNCH SCRUBS : None PAD RPO3 - 26 PLT: LAUNCH WINDOW : DEORBIT BURN : 104.5 SEP 1 : DEPLOYED: FRC3 - 25 2H30M CTOB 311:15:52:54Z 125 LBS 39B-39 Steven W. Lindsey SLWT-2 2:23:46:30 LAUNCH DELAYS : (Flt 2 - STS-87) ACTUAL: MET MLP-2 EOM PLS : KSC XRANGE: 172 NM NON - DEPLOYED : - Held for 9 minutes 36 seconds during T-9 minute hold to P540/R229/V131/M200 100/104.5/ SLWT 302.2 X 294 understand the cause of the three master alarms (MA) TAL: BYD ORBIT DIR : DL 44 24108 LBS TAL WX : BEN, MRN 104.5/72/ RPT NM during cabin leak checks. First MA was cabin P reached M / S 1 : AIM PT : NOMINAL 104.5 MAX: MIDDECK: 15.35 psi during cabin leak check. Two MA’s were Stephen K. Robinson SELECTED: 283K SEP 2 : 1314 LBS differential pressure/differential time alarms. It was (Flt 2 – STS-85) RTLS: EDW 15/N/SF MLGTD: 3243 FT 1 = 2048 (1) MIN: 3:06:16:40 concluded that the alarms were expected and count was SHUTTLE P541/R222/V152/M196 TAL: BYD 32/N/SF 311:17:03:30Z 2 = 2043 (2) 215K MET resumed. AOA: EDW 22 VEL: 199 KGS ACCUMULATED - Held for 9 minutes 58 seconds at T-5 minutes for PLS: EDW 22/CI/N 196 KEAS 3 = 2045 (2) WEIGHTS: range safety hold call for two intruder aircraft in Launch M / S 2 : HDOT: -1.0 FPS SLWT TI: DEPLOYED: Danger Area. Resumed count but two calls were made Scott E. Parazynski TDEL: ALL BLOCK IMPACT 5:22:01:37 850155 LBS to hold at T-31 seconds, one for engine 2 pitch position (Flt 3 - STS-66, STS-86) -0.03 -0.108/0.07 TD NORM 205 : II A ENGINES 1:28:02 MET NON - DEPLOYED : NO GO and the second for range safety NO GO. These 2559 FT P542/R187/V145/M164 MET 301.5 X 293.5 1378355 LBS holds were removed before count reached T-31 MAX Q NAV : DRAG CHUTE LAT: NM CARGO TOTAL : seconds; hence, no additional delay. M / S 3 : 755 765 DEPLOY : 20.8°N 2824652 LBS NOT USED TAL WX : Pedro Duque SRB STG : LONG: PERFORMANCE (ESA-Spain) 147.2°W - Banjul, Ben Guerir, and Moron were forecast and 2:03.7 2:03 NLGTD: 6248 FT MARGINS ( LBS ) : observed GO. Banjul was prime and selected. P543/R245/M213 311:17:03:40Z FPR: 3783 PERF: NOMINAL VEL: 164 KGS FUEL BIAS: 720 DOLILU / I - LOADS : FINAL TDDP: 1587 P / S 1 : 164 KEAS - DOLILU II uplink # 23, I-Load uplink # 42. 2 ENG TAL ( BYD ) : HDOT: -6.6 FPS RECON: 2740 Chiaki Mukai 2:11 2:13 (Japan) BRK INIT : 138 KGS PAYLOADS: PERFORMANCE ENHANCEMENTS : (Flt 2 - STS-65) NEG RETURN : 8726 FT PLB: - Standard set plus PE High Q. P544/R181/V153/F23 3:45 3:52 SPACEHAB DRAG CHUTE (Single) FLIGHT DURATION CHANGES : None P / S 2 : PTA ( U / S 500) : JETTISON: HOST NOT USED Senator John H. Glenn (2) 4:12 4:08 SPARTAN–201 FLIGHT RULE WAIVER : 2 (Deploy & Retrieve) - Forecast at deorbit burn time was a maximum P545/R246/M214 DROOP: BRK DECEL FPS : M 3 EOM AVE 5.8 PK 7.8 (Solar Wind Exp.) crosswind of 16 knots. Flight rule limit is 15 knots. 5:21 GAS (2) Observed crosswind < 10 knots. Landed on orbit 135. WHEELS STOP : WEIGHT: IEH-3 (PANSAT) PTM ( U / S 500) : 311:17:04:30Z 228455 LBS (Deployed) FIRSTS / LASTS / RECORDS : 5:13 5:06 12751 FT - First flight using High Q flight design. X CG: MIDDECK: MECO CMD : - First flight with three Block IIA SSME’s (Rocketdyne ROLLOUT: 1076.83 DEORBIT PCG-STES HPFTP). 8:20.7 8:21.6 9508 FT SAREX-II 60 SECS ALT: BRIC - John Glenn’s first flight was Mercury-Atlas 6 on MCC WHITE FCR (22) VI: LANDING: 301.5 X 285.9 2/20/62. 26102 26092 WINDS: NM 5 CYRO TK SETS - Glenn’s age at first flight 40Y7.5M, second flight FLIGHT DIRECTORS : 0H, 10R KTS WEIGHT: 5 GN2 TANKS 77Y4M, 36Y8.5M between flights. A/E - L. J. Ham OMS -2 : OFFICIAL: 228388 LBS VELOCITY - First flight using space-to-space comm system (as 41:57 41:57 0609P14 DTO). LD/O1 - P. L. Engelauf 5.02 FPS 5.02 FPS T0, R9 KTS 26063 FPS O 2 - P. S. Hill X CG: - Second flight of Super Lightweight Tank (SLWT). O 3 - P. F. Dye 1078.45 ENTRY MOD - J. W. Bantle RANGE Continued… Continued… Continued… 4290 NM Revision S May 2002 SPACE SHUTTLE MISSIONS SUMMARY Page 112 - STS-95 CREW LANDING SITE/ SSME-TL (7) LAUNCH SITE, RUNWAY, NOM- SRB ORBIT PAYLOAD MISSION HIGHLIGHTS FLT ORBITER LIFTOFF TIME, CROSSRANGE ABORT RSRM FSW WEIGHTS, (LAUNCH SCRUBS/DELAYS, EMERG NO. TITLE, NAMES LANDING SITES, LANDING TIMES THROTTLE AND INC HA/HP PAYLOADS/ TAL WEATHER, ASCENT I-LOADS, & EVA'S ABORT TIMES FLT DURATION, PROFILE ET EXPERIMENTS FIRSTS, SIGNIFICANT ANOMALIES, ETC.) WINDS ENG. S.N. STS-95 Continued… Continued… Continued… DENS ALT : 965 FT RMS 51 EVENTS : Continued FLT DURATION : (S.N. 201) - SPARTAN-201 release 305:19:00:12Z, 2:23:40:36 8:21:43:56 RMS used for MET. SPARTAN-201 - Due to drag chute anomaly, drag chute was not armed S / T : 790:03:08:16 deploy, retrieve and and deployed. berth, ACVS, - Inert weight adjustment -200 lbs included in STS OPR OV -103 : OSVS, and VGS chargeable. 186:13:31:48 OPS. - SPARTAN capture 307:20:47:49Z, 5:01:28 MET. DISTANCE: Berth 5:01:46 MET. 3,644,459 sm RENDEZVOUS # 43 : - Deployed, separated, rendezvoused with SPARTAN- 201. RADIATOR DEPLOY # 23 - Both port and starboard panels deployed. SIGNIFICANT ANOMALIES : - Low Iodine Residual System (LIRS) large spraying leak. Used backup galley iodine removal system. - Unpleasant taste (rubber hose) from LIRS. - During space-to-space comm tests, no data from EMU 1 in primary. - Drag chute door fell off during ME throttle up at T-5 seconds; hence, not deployed during landing. - Decision made to disable chute for STS-88. - WSB 2 overcooled six times during entry. - SPARTAN ground command problem. - RCS jet L3L failed off, then failed leak..