1985-059A
Bion 7 carried the macaques Verny and Gordy for cardiovascular and biorhythm studies. The 10 pregnant rats included at least one giving birth to a litter in flight.
| Bion 7 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1985 Jul 10 | 0315 | Launch by Soyuz-U | PL |
| 0317 | Blok-BVGD sep | ||
| 0319 | Blok-I burn | ||
| 0324 | Blok-I sep | ||
| 1985 Jul 10 | 211x267x82.4 | ||
| 1985 Jul 14 | 212x270x82.4 | ||
| 1985 Jul 16 | 211x268x82.4 | ||
| 1985 Jul 17 | 0016? | Deorbit | |
| 0026? | PO sep | ||
| 0032? | Entry | ||
| 0046? | Landed | ||
1964-F10
The first Titan IIIA was launched on 1964 Sep 1 from Cape Kennedy. It carried a 1414 kg dummy payload. The Transtage burn cutoff prematurely and the vehicle did not reach orbit. The Transtage and nosecone reentered uprange from Ascension Island.
Planned Transtage burn was 406s, cutoff came after 391s. For a 406s burn we expect 9500 kg burned, giving final mass of 4450 kg if total mass at MES was 13950 kg; then dV = 3.485 km/s. If planned velocity was 7.808 km/s (160 x 160 km) then initial orbit is 4.323 km/s ( -5542 x 160 km). After 391s we have 9150 kg burnt giving 4800 kg left, with dV = 3.254 km/s + 4.323 km/s = 7.577 km/s or -560 x 160 km, not so far from orbit. Such a orbit predicts (ignoring drag) reentry at around 10N 35W which is well uprange from Ascension.
| Transtage 2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1964 Sep 1 | 1500 | Launch by Titan IIIA | CK LC20 |
| 1502? | T+2:30? St 1 sep | ||
| 1505? | T+5:33? St 2 sep | ||
| 1505? | T+5:33? Transtage MES | ||
| 1512? | T+12:05? Transtage cutoff | ||
| 1517? | Impact Atlantic | ||
1987-003A
| Kosmos-1812 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1987 Jan 14 | 0905:00 | Launch by 11K68 | Plesetsk 41.14E |
| T+2:00 St 1 sep | |||
| T+3:33? GO sep | |||
| T+4:38? St 2 sep | |||
| T+5:20? S5M burn 1 | |||
| 0911 | T+6:48 S5M MECO1 km | 60? x 650 x 82.5 | |
| T+40:58? S5M burn 2 | |||
| T+41:08? S5M MECO2 | |||
| 0946? | T+41:38? S5M sep | ||
| 1987 Jan 14 | 629x665x82.6 | ||
| 1987 Mar 6 | 634x664x82.5 | ||
1986-020A
| Kosmos-1734 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1986 Feb 26 | 1340 | Launch by Soyuz | PL |
| 1348 | Blok-I sep | ||
| 1986 Feb 26 | 89.63 167 x 345 x 67.1 | ||
| 1986 Mar 5 | 89.17 158 x 307 x 67.1 | ||
| 1986 Mar 6 | Orbit raise | 89.67 169 x 346 x 67.1 | |
| 1986 Mar 8 | 89.55 168 x 335 x 67.1 | ||
| 1986 Mar 8 | Orbit raise | 89.99 177 x 370 x 67.1 | |
| 1986 Mar 18 | SpK-1 fiducial | ||
| 0530? | Deorbit | ||
| 0540? | Entry | ||
| 0552? | Landed | ||
| 1986 Mar 20 | 89.28 168 x 308 x 67.1 | ||
| 1986 Mar 20 | Orbit raise | 89.45 173 x 321 x 67.1 | |
| 1986 Mar 27 | 89.02 167 x 284 x 67.1 | ||
| 1986 Mar 27 | Orbit raise | 89.38 180 x 306 x 67.1 | |
| 1986 Apr 4 | 88.98 175 x 272 x 67.1 | ||
| 1985 Apr 4 | Orbit raise | 89.68 178 x 339 x 67.1 | |
| 1985 Apr 7 | SpK-2 fiducial | ||
| 2241? | deorbit | ||
| 2251 | Entry | ||
| 2303? | Landed | ||
| 1986 Apr 10 | 89.40 175 x 313 x 67.1 | ||
| 1986 Apr 10 | Orbit raise | 89.99 178 x 368 x 67.1 | |
| 1986 Apr 19 | 89.58 176 x 331 x 67.1 | ||
| 1986 Apr 19 | Orbit raise | 90.14 177 x 384 x 67.1 | |
| 1986 Apr 26 | 0220 | 89.87 177 x 358 x 67.1 | |
| 1986 Apr 26 | 1826? | C,D ejected | |
| 1986 Apr 26 | reentered after 59d | ||
| 1850? | Deorbit | ||
| 1903? | Entry | ||
| 1915? Landed | |||
1978-037A
Two-tone telemetry?; Med res satellite
| Kosmos-1002 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1978 Apr 6 | 0910 | Launch by Soyuz-U | Baikonur |
| 0914 | Blok-I burn | ||
| 0918 | Blok-I sep | ||
| 1978 Apr 6 | 89.41 206 x 283 x 65.1 | ||
| 1978 Apr 18 | 89.13 197 x 265 x 65.0 | ||
| 1978 Apr 19 | |||
| 0457? | Deorbit | ||
| 0507? | PO sep | ||
| 0513? | Entry | ||
| 0528? | Landed | ||
1975-122A
Prognoz-4 was launched in Dec 1975 with its apogee over the sunward hemisphere. The SO-M bus was similar to SO but with improved systems.
| Prognoz-4 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1975 Dec 22 | 0208 | Launch by Molniya-M | KB |
| 0216 | Blok-I MECO | ||
| 0216 | Blok I sep | ||
| 0309? | Blok-L burn | ||
| 0313? | Blok-L MECO | ||
| 0313? | Blok-L sep | ||
| 1637 | Pass EL1:4 | ||
| 1975 Dec 23 | 5740.0 634 x 199000 x 65.0 (RAE) | ||
| 1979 Mar 25 | end of ops | ||
1984-043A
| Kosmos-1550 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1984 May 11 | 0619 | Launch by 11K65M | Plesetsk |
| T+2:10 St 1 MECO | |||
| T+2:12 St 1 sep | |||
| T+2:12 St 2 burn 59km | |||
| T+2:27 Fairing sep 76km | |||
| 0627? | T+8:03 St 2 MECO 150 km | 150 x 1003? x 83 | |
| T+1:02:19 St 2 MES2 | |||
| T+1:02:30 St 2 MECO2 | |||
| 0722? | T+1:02:50 St 2 sep | ||
| 1984 Jun 5 | 105 993x1025x83.0 | ||
1971-108A
While Kosmos-463 was completing its mission, a replacement rocketed to orbit as Kosmos-464. This flight was also short, being recovered after only six days. The mission was launched from Plesetsk to a 72.9 deg orbit.
| Kosmos-464 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1971 Dec 10 | 1100:00 | Launch by 11A57 | PL |
| 1104 | Blok-I burn | ||
| 1108 | Blok-I sep | ||
| 1218 | 90.30 204 x 373 x 72.9 | ||
| 1971 Dec 11 | 0000 | 90.34 206 x 375 x 72.84 (RAE) | |
| 1971 Dec 12 | 0929 | 90.34 203 x 377 x 72.9 | |
| Lower orbit | |||
| 1971 Dec 13 | 1702 | 89.40 179 x 310 x 72.9 | |
| 1971 Dec 14 | 2130 | 89.23 178 x 293 x 72.86 (RAE) | |
| 1971 Dec 15 | Engine sep (108E) | ||
| 1971 Dec 16 | 0303 | 89.17 175 x 291 x 72.9 | |
| 0726? | Retrofire | ||
| 0736? | PO sep | ||
| 0741? | Entry | ||
| 0756? | Landed | ||
1986-021A
Kosmos-1735 was the first of a new series designed by KB Arsenal (rather than being produced under its technical direction based on the older NPOM design). RCS was 29m2.
| Kosmos-1735 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1986 Feb 27 | 0144 | Launch by 11K69 | Baikonur |
| 0146 | Stage 1 sep | ||
| 0148 | Stage 2 sep | ||
| 0232? | AKM burn | ||
| 1986 Feb 27 | 110x398x65.0 | ||
| 1986 Feb 27 | 406x425x65.0 | ||
| 1986 Apr 9 | 406x418x65.0 | ||
| 1986 Jun 23 | 404x417x65.0 | ||
| 1986 Aug 5 | 404x418x65.0 | ||
| 1987 Feb 15 | 404x418x65.0 | ||
| 1987 Apr 20 | 92.77 404x417x65.0 | ||
| 1987 Apr 21 | 93.19 427x435x65.0 | ||
| 1987 Apr 21 | 93.31 430x443x65.0 | ||
| 1987 Jul 14 | 93.30 429x443x65.0 | ||
| 1987 Sep 26 | mv up | ||
| 1987 Nov | decay begins | ||
| 1988 Feb 14 | 412x438x65.0 | ||
| 1988 May 20 | 396x426x65.0 | ||
| 1988 Oct 20 | 315x340x65.0 | ||
| 1988 Nov 17 | 87.74 158x167x65.0 | ||
| 1988 Nov 19 | reentered | ||
1981-121A
| Kosmos-1330 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1981 Dec 19 | 1150 | Launch by Soyuz | KB |
| 1158 | Blok I sep | ||
| 1981 Dec 19 | 90.00 168x381x70.4 | ||
| 1981 Dec 25 | 89.69 168x350x70.4 from 89.63 163x349 | ||
| 1981 Dec 30 | 89.88 167x368x70.4 from 89.22 162x308 | ||
| 1982 Jan 4 | 89.78 165x361x70.4 from 89.34 159x324 | ||
| 1982 Jan 10 | 90.04 166x386x70.4 from 89.03 155x298 | ||
| 1982 Jan 19 | 88.92 152x290x70.4 | ||
| 1982 Jan 19 | 0712 | reentered | |
1987-087A
| Kosmos-1891 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1987 Oct 14 | 1235:32 | Launch by 11K65M | Plesetsk 42.29E |
| T+2:10 St 1 MECO | |||
| T+2:12 St 1 sep | |||
| T+2:12 St 2 burn 59km | |||
| T+2:27 Fairing sep 76km | |||
| 1243? | T+8:03 St 2 MECO 150 km | 150 x 1003? x 83 | |
| T+1:02:19 St 2 MES2 | |||
| T+1:02:30 St 2 MECO2 | |||
| 1338? | T+1:02:50 St 2 sep | ||
| 1987 Oct 14 | 104.92 953x1028x82.9 | ||
