Friday, September 25, 1987
Kosmos 1032
1978-088A
Two-tone telemetry?; Hi res satellite with 25KS capsule.
| Kosmos-1032 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1978 Sep 19 | 0805 | Launch by Soyuz-U | Plesetsk |
| 0809 | Blok-I burn | ||
| 0813 | Blok-I sep | ||
| 1978 Sep 19 | 88.88 214 x 223 x 81.4 | ||
| 1978 Sep 30 | 88.52 200 x 202 x 81.3 | ||
| 1978 Oct 1 | 25KS capsule separated | ||
| 1978 Oct 2 | |||
| 0330? | Deorbit | ||
| 0340? | PO sep | ||
| 0346? | Entry | ||
| 0402? | Landed | ||
Kosmos 20
1963-040A
Zenit-2 No. 13 flew an 8-day mission in Oct 1963. The mission was successful and was the last OKB-1 Zenit-2.
| Kosmos-20 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1963 Oct 18 | 0930 | Launch by Vostok 8A92 | KB |
| 0934 | Blok-A sep | ||
| 0939 | Blok-E sep | ||
| 206 x 311 x 65.0 (TASS) | |||
| 205 x 302 x 64.9 (RAE) | |||
| 89.50 202 x 297 x 65.0 | |||
| 1963 Oct 26 | 0650? | Deorbit | |
| 0710? | Landed | ||
Thursday, September 24, 1987
Interkosmos 8
1972-094A
DS-U1-IK No. 2 (Interkosmos-8) was launched on 1972 Nov 30 by Kosmos-2 (11K63) from Plesetsk to study the polar ionosphere. It remained in orbit until Mar 1973.
Interkosmos-8 carried an ionospheric beacon and plasma detectors, provided by the DDR, the Soviet Union, the Czechoslovak Soviet Socialist Republic and the Bulgarian People's Republic.
Mass was 287 kg.
| Interkosmos-8 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1972 Nov 30 | 2150 | Launch by 11K63 Kosmos-2 | NIIP-53 |
| 2152 | S1 burn | ||
| 2200? | S1 sep | ||
| 93.1 204 x 649 x 71.0 | |||
| 1973 Feb 1 | End of operations | ||
| 1973 Mar 2 | Reentered | ||
Payload:
- Ionospheric beacon
- Langmuir probe
Sunday, September 20, 1987
Monday, September 14, 1987
Friday, September 11, 1987
Friday, September 4, 1987
Gambit-3 16
1968-074A
KH-8 16 (GAMBIT Mission 4316) was launched 1968 Sep 10 by Titan 3B Agena D from Vandenberg on a 15 day flight which epxerimented with color photography and tested an improved roll joint. It also introduced the RACS backup attitude control system, which was tested during the solo mission.
\peterfig{6}{01879s}
| KH-8 16 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1968 Sep 10 | 1830 | Launch by Titan 3B Agena D | V SLC4W |
| 1832? | Titan stage 1 sep | ||
| 1832? | Titan stge 2 sep | ||
| 1835? | Agena burn | ||
| 1840? | Agena MECO | ||
| 1968 Sep 10 | 1930 | 89.93 129 x 412 x 106.0 | |
| 1968 Sep 13 | 1917 | 89.44 122 x 370 x 106.1 | |
| 2047 | 89.95 135 x 407 x 106.1 | ||
| 1968 Sep 15 | 2041 | 89.59 126 x 381 x 106.0 | |
| 1968 Sep 17 | 1903 | 89.82 129 x 402 x 106.0 | |
| 1968 Sep 20 | 2217? | SRV deorbit rev 163 | |
| 1968 Sep 21 | 0805 | 89.07 117 x 338 x 106.0 | |
| 2000 | 89.29 138 x 339 x 106.0 | ||
| 1968 Sep 23 | 1638 | 89.12 142 x 320 x 106.0 | |
| 1968 Sep 25 | |||
| 2238? | SRV-1 ejected | ||
| 2245? | Entry | ||
| 2310? | SRV-1 recovered | ||
| 1400? | Deboost rev 238 | ||