Monday, November 29, 1993
Sunday, November 28, 1993
STS-9 (Columbia)
1983-116A
Columbia's 6th flight was the first Spacelab mission. It was launched on 1983 Nov 28 into a 249 x 250 km orbit. At 1942 on Nov 28 the hatch to the Spacelab module was opened for the first time.
On Dec 8, as the RCS jets were tested in preparation for retrofire, one of the GPC computers crashed. Deorbit was delayed after another computer crashed, although it was later restarted. The deorbit burn was sucessful, but at 2345, only 2 minutes before landing, fire broke out in the APUs in the rear fuselage. Despite the close shaves, Columbia landed safely and the fires went out.
A few months after the STS-9 mission, Columbia was transferred back to California for a major refit.
| STS-9 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1983 Jul 2 | Begin processing | ||
| 1983 Sep 23 | Rollover | VAB/3 | |
| 1983 Sep 28 | ET mate | ||
| 1983 Sep 28 | Rollout | LC39A | |
| 1983 Oct 17 | Rollback | VAB/3 | |
| 1983 Oct 19 | Demate, rollover | OPF | |
| 1983 Nov 3 | Rollover | VAB/3 | |
| 1983 Nov 7 | ET mate | ||
| 1983 Nov 8 | Rollout | LC39A | |
| 1983 Nov 28 | 1600:00 | Launch | LC39A |
| 1602:06 | SRB sep, 49.3 km | ||
| 1608:29 | MECO, 113.5 km | ||
| 1608:47 | ET sep, 115.4 km | 86.67 29 x 189 x 57.0 (dV) | |
| 1610:29 | OMS 1 (1:04) 33.8m/s | 83 x 250 | |
| 1611:33 | OMS-1 CO | 87.80 81 x 249 x 57.0 (dV) | |
| 1630 | ET apogee 189 km | ||
| 1640:37 | OMS 2 (1:41) 49.8m/s | ||
| 1642:19 | OMS 2 CO | ||
| 1701 | ET-11 reentry | ||
| 1729 | PLBD open | 89.49 243 x 255 x 57.0 | |
| 2031 | SL-1 activation complete | ||
| 2115 | RCS | ||
| 1983 Nov 29 | 0159 | 89.47 242 x 253 x 57.0 | |
| 1983 Nov 30 | 0311 | To cold attitude | |
| 1983 Nov 30 | 1239 | 89.45 242 x 252 x 57.0 | |
| 1983 Dec 1 | 0230 | End of cold soak | |
| 1983 Dec 2 | 1646 | 89.37 238 x 248 x 57.0 | |
| 1983 Dec 5 | 1443 | 89.27 235 x 241 x 57.0 | |
| 1825 | Hot soak test | ||
| 1983 Dec 6 | 0126 | End of hot soak | |
| 1983 Dec 6 | 1858 | 89.25 233 x 240 x 57.0 | |
| 1983 Dec 8 | RCS tests | ||
| 0936 | SL-1 deactivated | ||
| 1110 | GPC-1 computer failed | ||
| 1116 | GPC-2 computer failed | ||
| 1335 | GPC-2 restarted | ||
| 1642 | IMU-1 failed | ||
| 2252:00 | OMS DO (156s) 81.4m/s | ||
| 2254:36 | OMS DO CO | ||
| 2316:00 | Entry | ||
| 2347:24 | Landed | RW17 EAFB | |
| 2347:38 | NGTD | ||
| 2348:17 | Wheels stop | ||
| 2354 | APU-1 failed | ||
| 2358 | APU-2 failed | ||
| 1983 Dec 14 | 1655 | SCA | Biggs AAF, TX |
| 1983 Dec 14 | SCA | Kelly AFB TX | |
| 1983 Dec 15 | SCA | Eglin AFB FL | |
| 1983 Dec 15 | 1953 | SCA arr. | KSC |
| 1983 Dec 16 | Rollover | OPF | |
| 1984 Jan 26 | SCA | Kelly AFB TX | |
| 1984 Jan 27 | SCA | Edwards | |
| 1984 Jan 28 | Road transfer | Palmdale | |
| 1984 Jan 31 | Begin OMDP | ||
Friday, November 26, 1993
Kosmos 372
1970-083A
Kosmos-371 was a standard Tsiklon mission, transmitting signals at 149 MHz.
| Kosmos-371 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1970 Oct 12 | 1357:00 | Launch by 11K65M | PL |
| 1359? | Stage 2 burn | ||
| 1405? | Stage 2 coast | ||
| 1452? | Stage 2 burn 2 | ||
| 1452? | Stage 2 sep | ||
| 1970 Oct 28 | 0700 | 99.92 750 x 758 x 74.0 | |
Wednesday, November 24, 1993
Thursday, November 18, 1993
Molniya 166
1985-103A
Molniya-1 (F72, N66) was launched on 1985 Oct 27 from Plesetsk, within a few days of the previous Molniya-1 launch from Baikonur.
| Molniya-1 F72 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1985 Oct 28 | 1724:58 | Launch by 8K78M | PL |
| BVGD sep | |||
| GO sep | |||
| T+4:46 Blok A sep | |||
| T+4:56 KhO sep | |||
| T+8:46 Blok-I MECO | |||
| 1733 | T+8:50 Blok-I sep | ||
| T+53:16 BOZ burn | |||
| 1819? | T+53:56 BOZ sep | ||
| ML burn | |||
| T+56:46 ML MECO | |||
| 1822? | T+56:54 ML sep | ||
| 1985 Oct 28 | 460 x 39132 x 62.8 | ||
Molniya 131
1975-079A
Molniya-1 (F36, N31) was launched on 1975 Sep 2 into the C plane. It replaced F33.
| Molniya-1 F36 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1975 Sep 2 | 1309 | Launch by 8K78M | PL |
| BVGD sep | |||
| GO sep | |||
| T+4:46 Blok A sep | |||
| T+4:56 KhO sep | |||
| T+8:46 Blok-I MECO | |||
| 1317 | T+8:50 Blok-I sep | ||
| T+53:16 BOZ burn | |||
| 1402? | T+53:56 BOZ sep | ||
| ML burn | |||
| T+56:46 ML MECO | |||
| 1405? | T+56:54 ML sep | ||
| 1975 Sep | 736.7 623 x 40667 x 62.9 | ||
| 1975 Sep | 717.8 606 x 39749 x 62.9 | ||
| 1986 Nov 19 | Reentered | ||
Intelsat 402
1971-006A
The first Intelsat IV, F-1, was kept in storage until 1975. F-2 was the first to be launched, and was primary Atlantic satellite from 1971 to Sep 1973 when it was replaced by F7. It remained over the Atlantic in a backup role until it was switched off in 1983.
| Intelsat IV F-2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1971 Jan 26 | 0036:03 | Launch by Atlas Centaur | CC LC36 |
| T+2:32 BECO | |||
| T+2:35 Booster sep | |||
| T+3:17 Insulation panels | |||
| T+3:58 SECO, VECO | |||
| 0040 | T+4:01 Atlas sep | ||
| T+4:12 Centaur MES-1 | |||
| T+4:24 Fairing | |||
| 0046 | T+10:18 Centaur MECO-1 | 109.83 185 x 2252 x 29.4 | |
| 0100? | T+24? Centaur MES-2 | ||
| 0101? | T+25? Centaur MECO-2 | ||
| 0104 | T+28:47 Centaur sep | 640.52 547 x 35924 x 28.2 | |
| 0700? | Apo 1 | ||
| 1800? | Apo 2 | ||
| 1971 Jan 27 | 0330? | Apo 3 over 125E | |
| 1971 Jan 27 | 0344 | AKM 3.6W/d | |
| 1971 Mar 26 | Operational, AOR Primary with III F7 | GEO 24.5W | |
| 1971 Apr 22 | 1436.34 35785 x 35797 x 0.5 GEO 34.3W+0.07E | ||
| 1971 Oct 25 | 1436.04 35775 x 35796 x 0.1 GEO 23.4W | ||
| 1972 | AOR Primary | ||
| 1973 Sep | Replaced by IV F7 | ||
| 1975 Dec | GEO 19W (Morgan) | ||
| 1976 Feb | AOR Backup | GEO 1W | |
| 1977 Feb 26 | 1435.98 35770 x 35798 x 0.02 GEO 5.1W | ||
| 1977 Dec | GEO 4W (Morgan) | ||
| 1978 Mar 27 | 1436.13 35781 x 35793 x 0.82 GEO 4.8W | ||
| 1978 Sep | AOR Backup | GEO 4W | |
| 1979 Apr | Available as backup | GEO 6W | |
| 1979 Oct | mv in | GEO 4W | |
| 1979 Oct 12 | 1435.93 35777 x 35789 x 1.9 GEO 3.6W | ||
| 1980 Mar 3 | 1436.02 35779 x 35790 x 2.2 GEO 3.7W | ||
| 1980 May | mv out | GEO 4W | |
| 1980 May | mv in | GEO 1W | |
| 1980 May 30 | 1436.02 35773 x 35796 x 2.3 GEO 0.4W | ||
| 1982 Aug 9 | mv out | GEO 1W | |
| 1982 Aug 27 | 1435.97 35776 x 35792 x 4.0 GEO 0.5E | ||
| 1982 Oct | Engineering tests | GEO 3E | |
| 1982 Dec 19 | 1436.27 35766 x 35813 x 4.3 GEO 3.83E | ||
| 1983 May 10 | 1435.89 35752 x 35812 x 4.6 GEO 4.6E | ||
| 1983 May 11 | Orbit raise 300 km | 35969 x 36009 | |
| 1983 May 11 | Decommissioned | ||
| 1983 May 12 | 1446.26 35965 x 36005 x 4.6 | ||
| 1985 Nov 16 | 1456.88 36121 x 36261 x 6.7 | ||
| 1986 Dec 3 | 1456.90 36125 x 36259 x 7.6 | ||
| 1998 Aug 5 | 1456.96 36115 x 36272 x 15.1 | ||
Tuesday, November 16, 1993
Monday, November 15, 1993
Nova 3
1984-110A
Nova 3 (NNS 30500) was launched in Oct 1984. Its mass was 120 kg (or 166 kg).
Mass 173 kg (MOR). Mass at St 4 burnout 210 kg; St 4 ignition 486 kg. Conclude St 4 is mass 313 full 37 empty.
1.1m high 0.52m dia cyl bus with 4 panels and 79.2m gravity boom. Despin via magnets?
| Nova 3 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1984 Oct 12 | 0143:34 | Launch by Scout | V SLC5 |
| T+1:23 St 1 burnout | |||
| 0145:02 | T+1:28 St 1 sep | ||
| 0145:09 | T+1:35 St 2 burn | -6302 x 63 x 76.9 | |
| 0145:40 | T+2:06 St 2 burnout | ||
| 0146:10 | T+2:36 St 2 sep | -5831 x 166 x 86.3 | |
| 0146:14 | T+2:40 Fairing sep | -5831 x 166 x 86.3 | |
| 0146:16 | T+2:42 St 3 burn | ||
| 0147:04 | T+3:30 St 3 burnout | -4040 x 339 x 89.1 | |
| T+7:30 St 1 impact | |||
| 0151:35 | T+8:01 St 3 sep | ||
| 0151:40 | T+8:06 St 4 burn, 33s | -4040 x 335 x 89.1 (MOR) | |
| 0152:13 | T+8:39 St 4 burnout | 334 x 1007 x 90.0 (MOR) | |
| 0155? | St 4 sep | ||
| T+11:16 St 2 impact 121.3W 24.2N | |||
| T+19:02 St 3 impact at 123.0W 1.63S | |||
| 1984 Oct 13 | Activate DISCOS | 323 x 1053 | |
| Orbit raise | 357 x 1064 | ||
| 1984 Oct 15 | 102.21 648 x 1076 x 89.8 | ||
| 1984 Oct 16 | 104.32 818 x 1104 x 89.8 | ||
| 1984 Oct 17 | 1023 x 1157 x 89.9 | ||
| 1984 Oct 19 | 1160 x 1200 x 90.0 | ||
| 1984 Nov 10 | 0400 | Op frequency on | |
| 1993 Nov 8 | 0237 | Retired from service | |
Sunday, November 14, 1993
Kosmos 453
1971-090A
Kosmos-453 was a subgroup 1 DS-P1-Yu mission launched in Oct 1971 by 11K63 from Plesetsk.
| Kosmos-453 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1971 Oct 19 | 1240 | Launch by 11K63 | PL |
| 1242 | Stage 2 burn | ||
| 1247? | Stage 2 sep | ||
| 1971 Oct 26 | 0500 | 92.19 271 x 493 x 71.0 (RAE) | |
| 1972 Jan 1 | 0000 | 91.47 259 x 434 x 71.0 (RAE) | |
| 1972 Mar 3 | End of operations | ||
| 1972 Mar 19 | 0155? | Reentered | |
Interkosmos 18
1978-099A
The Magnetospheric Interkosmos (Mag-IK) satellite was launched on 1978 Oct 24 by Kosmos-3M from Plesetsk. The satellite was named Interkosmos-18 once in orbit. The lead science institute for the Interkosmos-18 project was IZMIRAN, the Institute of Terrestrial Magnetism and Aeronomy of the Academcy of Sciences. Interkosmos-18 carried a set of particles and fields instruments to study the magnetosphere in the 400 to 800 km altitude range. It also ejected the Czechoslovak satellite Magion to provide comparative data. Mag-IK operated until reentry in Mar 1981.
Mass was 990 kg.
| Interkosmos-18 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1978 Oct 24 | 1900 | Launch by 11K65M Kosmos-3M | NIIP-53 |
| 1902 | Stage 1 sep | ||
| Stage 2 burn | |||
| 1908? | Stage 2 MECO | ||
| 1930? | Stage 2 MECO-2 | ||
| 96.4 406 x 764 x 83.0 | |||
| 1981 Mar 15 | End of transmissions | ||
| 1981 Mar 17 | Reentered | ||
Payload:
- SG-R1 magnetometer
- Low energy particle flux
- Particle angular distances
- Electric and magnetic fields
- Double probe investigation of electrostatic fields
- Electron and ion densities and temperatures
Monday, November 8, 1993
Intelsat 405
1972-041A
The Intelsat IV F-5 satellite was placed over the Indian Ocean in 1972. It was the IOR Primary until around 1976 when it moved to a backup role. In 1980 it moved to the Pacific, staying there until 1981 when it was retired.
| Intelsat IV F-5 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1972 Jun 13 | 2153:04 | Launch by Atlas Centaur AC-29 | CC LC36 |
| T+2:32 BECO | |||
| T+2:35 Booster sep | |||
| T+3:17 Insulation panels | |||
| T+3:58 SECO, VECO | |||
| 2157 | T+4:01 Atlas sep | ||
| T+4:12 Centaur MES-1 | |||
| T+4:24 Fairing | |||
| 2203 | T+10:18 Centaur MECO-1 | ||
| 2218 | T+25:20 Centaur MES-2 | ||
| 2219 | T+26:33 Centaur MECO-2 | ||
| 2221 | T+28:47 Centaur sep | ||
| Payload orbit | 639.94 538 x 35903 x 27.00 (Flash) | ||
| T+31:37 Blowdown | |||
| T+35:46 End blowdown | |||
| Centaur orbit | 653.31 549 x 36575 x 27.00 (RAE) | ||
| 1972 Jun 14 | 0500? | Apo 1 | |
| 1500? | Apo 2 | ||
| 1972 Jun 15 | 0101 | AKM Apo 3 | GEO 124E dr |
1972 Jul | IOR Primary | GEO 61.4E | |
| 1975 | IOR Primary | GEO 61E | |
| 1975 Dec 30 | GEO 60.3E (Morgan) | ||
| 1977 Feb 24 | 1436.15 35786 x 35788 x 0.1 GEO 60.13E+0.00 | ||
| 1978 Sep 30 | IOR Backup | GEO 60.2E | |
| 1978 Oct 26 | 1436.04 35778 x 35792 x 0.0 GEO 60.2E+0.0 | ||
| 1978 Dec 21 | 1436.18 35780 x 35796 x 0.1 GEO 57.0E+0.0 | ||
| 1979 Jan 31 | GEO 57E | ||
| 1980 Apr 21 | 1436.01 35778 x 35791 x 0.1 GEO 57.8E+0.0 | ||
| 1980 May | mv out | GEO 57E | |
| 1980 May 25 | 1430.77 35572 x 35791 x 0.1 GEO 100.5E+1.3W | ||
| 1980 Jul 19 | 1431.17 35576 x 35803 x 0.1 GEO 171.4E+1.2W | ||
| 1980 Jul | mv in | GEO 179E | |
| 1980 Aug 8 | 1435.97 35780 x 35787 x 0.1 GEO 179.3E+0.0 | ||
| 1980 Oct 5 | 1436.05 35776 x 35794 x 0.1 GEO 178.8E+0.0 | ||
| 1981 Jun | GEO 179.2E+0.03 0.6 | ||
| 1981 Jun 17 | mv out | GEO 179E | |
| 1981 Jun 19 | 1435.92 35782 x 35784 x 0.6 GEO 179.5E+0.04 | ||
| 1981 Jul 24 | 1435.80 35779 x 35781 x 0.7 GEO 178.5W+0.07 | ||
| 1981 Sep 29 | 1435.46 35773 x 35775 x 0.8 GEO 170.7W+0.15 | ||
| 1982 Apr 19 | 1434.42 35745 x 35761 x 1.3 GEO 108.0W+0.42W | ||
| 1982 Jun | Drifting | GEO 87W | |
| 1982 Oct | Slow drift | GEO 39W | |
| 1982 Nov 4 | 1435.31 35757 x 35785 x 1.7 GEO 40.8W+0.19W | ||
| 1983 Jan 14 | 1436.33 35758 x 35823 x 1.9 GEO 39.6W+0.06E | ||
| 1983 Feb 23 | mv out | 1437.18 35789 x 35825 x 2.0 GEO 43.2W+0.3E | |
| 1983 May 10 | 1438.65 35820 x 35852 x 2.2 GEO 88.4W+0.6E | ||
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