OPERATIONS
Science Operations
DOY = day-of-the-year; FD = Flight date. Times are in UTC.
Month | Day | Year | DOY | FD | Time | Event | |
JAN | 7 | 1999 | 7 | 1133 | 22:40 | SK-12 (in ESR), Delta-V = -8.1 m/s, segment 1/2/3/4 = 5/15/28/15 min, fuel 8.6 kg | |
JAN | 8 | 1999 | 8 | 1134 | 15:47 | Gyro B Test | |
JAN | 8 | 1999 | 8 | 1134 | 19:58 | Start reduction of yaw rate | |
JAN | 15 | 1999 | 15 | 1141 | - | Reaction wheels spinning and maintenance | |
JAN | 19 | 1999 | 19 | 1145 | 18:30 | SK-13 (in ESR), Delta-V = - 8.6 m/s, segment 1/2/3: 20/30/20 min, fuel 9.2 kg | |
JAN | 20 | 1999 | 20 | 1146 | - | Roll Rate Determination a la Harris | |
JAN | 26 | 1999 | 26 | 1152 | 19:00 | SK-14 (in ESR), Delta-V =-3.9m/s ; segment 1/2/3 = 5/21/1 min, fuel 4.27 kg | |
JAN | 28 | 1999 | 28 | 1154 | - | Flight test of FPSS raw data processing | |
JAN | 29 | 1999 | 29 | 1155 | - | Preparation of ESR exit maneuver (ACU & SSU patches) | |
JAN | 30 | 1999 | 30 | 1156 | - | ESR exit maneuver | |
JAN | 30 | 1999 | 30 | 1156 | 17:45 | In RMW (Roll Angle -63 deg); mom mgt 21:10 | |
JAN | 30 | 1999 | 30 | 1156 | 22:57 | DHS Reconfiguration | |
FEB | 1 | 1999 | 32 | 1158 | 19:15 | SK-15 (in RMW), Delta-V = +0.32 m/s, segment 1/2 = 10/25 min; fuel: 0.27 kg | |
FEB | 1 | 1999 | 32 | 1158 | 22:12 | DHS Reconfiguration | |
FEB | 2 | 1999 | 33 | 1159 | 16:11 | Transition Tests RMW/NM | |
FEB | 2 | 1999 | 33 | 1159 | 19:12 | Back to Normal Mode | |
FEB | 5 | 1999 | 36 | 1162 | 15:59 | Tape Recorder Maintenance | |
FEB | 14 | 1999 | 45 | 1171 | 13:53 | ESR-11, by off-pointing | |
FEB | 18 | 1999 | 49 | 1175 | 18:52 | Back to Normal Mode (Roll Angle -120 deg), mom mgt 15:20 | |
MAR | 3 | 1999 | 62 | 1188 | 16:05 | Mom. Mgmt, 4 segments: yaw/roll/pitch/yaw; final speeds: 600/-750/600 rpm | |
MAR | 4 | 1999 | 63 | 1189 | 16:18 | Roll by 120 degrees to 0.653; roll trim to -0.109 degrees; 198 arcsec yaw off-set 23:03 | |
MAR | 4 | 1999 | 63 | 1189 | - | Loss of SSU Patch during S/C roll. | |
MAR | 5 | 1999 | 64 | 1190 | 17:35 | Mom. Mgmt, 3 segments: pitch/yaw/roll; final sppeds: 2000/2000/-2000 rpm; 20:05 done | |
MAR | 5 | 1999 | 64 | 1190 | 20:30 | SK-16, Delta V = -11.87 cm/sec; 4 segments: jets 1/2/4/6: 52/52/2/2 sec on-time | |
MAR | 5 | 1999 | 64 | 1190 | 21:30 | Mom. Mgmt, 3 segments: roll/yaw/pitch; final speeds: 3000/500/-1700 rpm, 22:30 done | |
MAR | 6 | 1999 | 65 | 1191 | 19:25 | SSU SEU Flag (Fail-over to no roll control); back to normal mode 20:00 | |
MAR | 8 | 1999 | 67 | 1193 | 16:00 | Roll trim by 1645 arcsec (0.45 degrees) for RSL activation at 17:25 | |
MAR | 13 | 1999 | 72 | 1198 | - | MDI Continuous Coverage, until June 14 at 01:50 UT | |
MAR | 15 | 1999 | 74 | 1200 | 16:48 | Roll trim by 378.86 arcsec (RSL correction) | |
MAR | 18 | 1999 | 77 | 1203 | - | SSU-A: heater for startracker head switched off | |
APR | 9 | 1999 | 99 | 1225 | - | RSL preparation on ground changed to skip pixel boundaries | |
APR | 29 | 1999 | 119 | 1245 | 19:09 | SSU SEU Flag (Fail-over to no roll control); back to Normal Mode 20:26 | |
MAY | 10 | 1999 | 130 | 1256 | - | MEDOC Campaign #3, run for 3 weeks until May 31, 1999 | |
MAY | 11 | 1999 | 131 | 1257 | 17:37 | Gyro B power off (all 3 gyros are off) | |
MAY | 18 | 1999 | 138 | 1264 | 14:00 | Mom. Mgmt, 3 segments: roll/pitch/yaw; final speeds: -581/762/1877 rmp; 17:00 done | |
MAY | 20 | 1999 | 140 | 1266 | 17:07 | SSU SEU flag (Fail-over to no roll control); back to Normal Mode 18:31 | |
JUNE | 11 | 1999 | 162 | 1288 | 19:49 | SSU Staircase Filter changed from 60 to 600 in AOCS Software | |
JUNE | 14 | 1999 | 165 | 1291 | 13:10 | Tape Recorder Maintenance | |
JUNE | 17 | 1999 | 168 | 1294 | 20:30 | SK-17, Delta V=0.46 m/sec; 3 segments; jets 2/3/4: 3.5/155/151 sec on-time | |
JUNE | 17 | 1999 | 168 | 1294 | 23:00 | Mom.Mgmt, 3 segments; roll/pitch/yaw; final speeds: -520/520/1900 rmp, 00:00 done | |
JULY | 6 | 1999 | 187 | 1313 | - | Increase Mv threshold when commanding search/track of new star | |
JULY | 15 | 1999 | 196 | 1322 | 04:00 | MDI Continuous Coverage, planned until July 20, 07:20 | |
AUG | 26 | 1999 | 238 | 1364 | 07:10 | MDI Continuous Coverage, planned until Sep 1, 02:45 UT | |
AUG | 27 | 1999 | 239 | 1365 | 12:33 | SSU SEU Flag (Fail-over to no roll control); back to Normal Mode 12:42 | |
SEPT | 24 | 1999 | 267 | 1393 | - | Gyroless Flight Comm: AOCS Software Part 1 upload | |
SEPT | 27 | 1999 | 270 | 1396 | - | Gyroless Flight Comm: AOCS Software Part 2 and COBS upload; test of CRP, RMW, NM | |
SEPT | 28 | 1999 | 271 | 1397 | - | Gyroless Flight Comm: star swap, P/Y/R profiles in NM, protection functions, Mom mgt. | |
SEPT | 29 | 1999 | 272 | 1398 | - | Gyroless Flight Comm: P/Y profiles in CRP, 1st part of 360 deg, roll: 8, 10 and 54 deg. | |
SEPT | 30 | 1999 | 273 | 1399 | - | Gyroless Flight Comm: final part of 360 deg. roll: 90, 105 and 90 deg. | |
OCT | 1 | 1999 | 274 | 1400 | - | Gyroless Flight Comm: SSU patch, profiles P/Y/R in RMW, fallback to CRP & recovery. | |
OCT | 2 | 1999 | 275 | 1401 | - | Gyroless Flight Comm: Mom. Mgt, RW4 maint., Mom. Mgt, SK-18 (delta V=0.05 m/sec) | |
OCT | 4 | 1999 | 277 | 1403 | - | Gyroless Flight Comm: test of routine ops (release guide star, RSL uplink, recover star) | |
OCT | 6 | 1999 | 279 | 1405 | - | MEDOC Campaign #4, run until October 17. | |
OCT | 13 | 1999 | 286 | 1412 | - | MDI Continuous, planned until October 19, 12:45 UT. | |
OCT | 21 | 1999 | 294 | 1420 | - | Tape Recorder Maintenance | |
NOV | 8 | 1999 | 312 | 1438 | - | Instrument Prep. for Leonids Begins | |
NOV | 9 | 1999 | 313 | 1439 | 20:34 | Mom. Mgmt, 3 segments: roll/pitch/yaw; final speeds: -600/800/1500 rpm, done 21:48 | |
NOV | 9 | 1999 | 313 | 1439 | 20:34 | MDI Continuous planned until November 16, 13:30 UT | |
NOV | 16 | 1999 | 320 | 1446 | 17:20 | Leonids roll in CRP: -113.42 deg. to position -120.992 deg.;TM in MR; SSR, SSU off | |
NOV | 19 | 1999 | 323 | 1449 | 14:39 | Leonids roll back in CRP: -114 deg. to position -6.12 deg.;TM in MR; done 18:30 | |
NOV | 19 | 1999 | 323 | 1449 | 22:16 | Mom. Mgmt, 1 segment: yaw; final speeds: 2106/1439/-2127 rpm, done 23:40 | |
NOV | 20 | 1999 | 324 | 1450 | 00:20 | SK-19, Delta V = 6.8 cm/sec; 4 segments: jets 1/2/4/6: 27.9/28.4/1/1.3 sec on-time | |
NOV | 20 | 1999 | 324 | 1450 | 01:00 | Mom. Mgmt, 2 segm: pitch/roll: speeds: 2986/511/-1285 rpm, Hx=10.52 Nms: done 01:45 | |
NOV | 22 | 1999 | 326 | 1452 | - | Instrument Recovery from Leonids Ends | |
NOV | 28 | 1999 | 332 | 1458 | 11:55 | ESR-12 triggered by ACU Reset Monitoring | |
NOV | 29 | 1999 | 333 | 1459 | 18:35 | Recovery to CRP, roll angle -125 deg | |
NOV | 30 | 1999 | 334 | 1460 | 01:13 | Mom. Mgmt, 2 segments: jets 5/2; final speeds: 2021/-2389/1967 rpm, done 23:40 | |
NOV | 30 | 1999 | 334 | 1460 | 16:20 | roll-back by 117.22 deg; to -7.219 deg; done 20:16 | |
DEC | 1 | 1999 | 335 | 1461 | 15:00 | Mom. Mgmt, 3 segments: jets 4/2/5; final speeds: 1750/1750/-1750 rpm, done 16:40 | |
DEC | 1 | 1999 | 335 | 1461 | 18:00 | SK-20, Delta V = 0.364 m/sec; jets 1/2/4/6; 148/151/5/6 sec on-time. | |
DEC | 1 | 1999 | 335 | 1461 | 18:09 | Guide star loss during station keeping; CRP mode fails to control the roll | |
DEC | 1 | 1999 | 335 | 1461 | 18:43 | ESR-13, triggered from ground; no roll control in CRP due to ACU TM buffer overrun | |
DEC | 2 | 1999 | 336 | 1462 | 19:42 | Recovery to CRP, roll angle -67.67 degrees | |
DEC | 8 | 1999 | 342 | 1468 | 06:55 | MDI continuous contact, planned until Dec 13 at 14 UT | |
DEC | 8 | 1999 | 342 | 1468 | 16:45 | Mom. Mgmt, 3 segments; jets 5/1/3; final speeds: 730/-1615/2485 rpm, done 17:42 | |
DEC | 8 | 1999 | 342 | 1468 | 19:52 | roll-back by 69.0 deg; to -7.25 deg; done 21:32 | |
DEC | 9 | 1999 | 343 | 1469 | 12:25 | Mom. mgmt, 2 segments: jets 4/2; final speeds: 1624/1622/-1690 rpm, done 13:48 | |
DEC | 9 | 1999 | 343 | 1469 | 14:05 | SK-21, delta v = 0.73 m/s; in 4 segm.; jets 1/2/4/6; final speeds: 1680/1357/-1493 rpm | |
DEC | 9 | 1999 | 343 | 1469 | 21:25 | Mom. mgmt, 3 segments: jets 4/1/5; final rpm's: 2790/609/-1292, done 23:12; Hx=10.1 Nms | |
DEC | 10 | 1999 | 344 | 1470 | 01:00 | Back in Normal Mode | |
DEC | 29 | 1999 | 363 | 1489 | 17:32 | UVCS closed door in anticipation of Y2K problems |