Friday, November 12, 1976
Thursday, October 28, 1976
Thursday, October 21, 1976
Wednesday, October 20, 1976
Thursday, October 14, 1976
Sunday, September 19, 1976
Wednesday, September 15, 1976
Tuesday, September 14, 1976
Corona 44
1962-026
KH-4 Mission 9037 was launched on 1962 Jun 23 by Thor Agena B from Vandenberg. It reached a 213 x 293 km x 75.1 deg orbit, lower than planned. The satellite carried the MURAL camera system and the Space Radio Project to measure celestial diffuse radio emission. To this point the HSRP flights detected only terrestrial interference. FTV 1129 also carried a number of ionospheric experiments which were intended to study the effects of the FISHBOWL atmospheric nuclear tests . The SRV was recovered after a two day flight.
| KH-4 Mission 9037 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1962 Jun 23 | 0030:47 | Launch by Thor Agena B | V Pad 4 |
| 0032 | Thor MECO (T+2:28) | ||
| 0032 | Thor VECO (T+2:37) | ||
| 0032 | Thor sep (T+2:47) | ||
| 0033 | Agena burn (T+3:14) | ||
| 0037:57 | Agena cutoff (T+7:10) | 209 x 315 x ? (VCR) | |
| 1962 Jun 23 | 0428 | 89.65 199 x 314 x 75.18 | |
| 1962 Jun 26 | 0228? | SRV ejected | |
| 1962 Jun 26 | 0241? | SRV recovered over Pacific on rev 49 | |
| 1962 Jun | 89.6 199 x 314 x 75.1 (SATCAT) | ||
| 1962 Jun 27 | 1200 | 89.58 213 x 293 x 75.1 (RAE) | |
| 1962 Jun 29 | 2010 | 89.27 209 x 267 x 75.1 | |
| 1962 Jul 3 | 2130 | 88.82 209 x 222 x 75.1 (RAE) | |
| 1962 Jul | 88.2 187 x 187 x 75.1 (SATCAT) | ||
| 1962 Jul 5 | 2253 | 88.24 187 x 187 x 75.1 | |
| 1962 Jul 7 | Last ionosphere data | ||
| 1962 Jul 7 | 1700? | CORONA/Agena reentered | |
Wednesday, September 1, 1976
Wednesday, August 25, 1976
Tuesday, August 24, 1976
Tuesday, August 17, 1976
Kosmos 173
1967-081A
The next DS-P1-Yu satellite, Kosmos-173 (DS-P1-Yu No. 8), was part of the main subgroup (Subgroup 1), with an inclination of 71 degrees and an apogee of 480 km.
| Kosmos-173 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1967 Aug 24 | 0500 | Launch by 11K63 | PL |
| Stage 2 burn | |||
| 0507? | Stage 2 sep | 92.1 277 x 480 x 71.0 | |
| 1967 Nov 3 | end of ops | ||
| 1967 Dec 17 | 1744? | Reentered | |
DMSP 3
1967-080A
The third Burner 2 launch, now carried out by Air Defense Command, went up on 1967 Aug 23 into an 834 x 892 km orbit from the Vandenberg pad, now renamed LE-6. It carried the F19 satellite which operated for 204 days for its primary mission, and transmitted for 3 years. F19 introduced system H, an IR radiometer similar to the Block 3 HRR.
| DSAP 03419 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1967 Aug 23 | 0441 | Launch by Thor Burner 2 | V LE-6 |
| 0443? | Thor sep | ||
| 0452? | Burner II burn | ||
| 0455? | Burner II sep | ||
| 102.2 834 x 892 x 99.0 | |||
Sunday, August 15, 1976
Explorer 11
1961-013
The 38 kg S-015 payload carried a Cerenkov detector to study gamma rays from space. Launched by a Juno II (AM-19E) from Cape Canaveral at 1416:38 on 1961 Apr 27, it reached a 487 x 1779 km x 28.8 deg orbit; the orbit was very close to the one planned. The satellite was a cylinder topped by a box, and remained attached to the stage 4 motor. Orbit mass was 43 kg including a 3 kg nutation damper weight. RTV motor is 0.15m dia 1.1m long with 5.8 kg empty mass, payload is 0.29m dia 1.1m long with 37 kg mass.
The telescope was tipped with a thin aluminium shield for micrometeorite protection which could be ejected on command. This shield is possibly the object 1961 nu 2 which was cataloged in Feb 1969.
S-15 was built by NASA MSFC; the gamma ray telescope was built at MIT. Management was by NASA GSFC.
Explorer XI, as it was now designated, transmitted until Dec 6. It did not detect significant gamma ray flux (about 22 photons were observed), and the true birth of orbital gamma ray astronomy had to wait until the COS-B mission in 1975. Explorer XI set an upper limit to the 50 MeV gamma ray background of 3x 10-4 photons/cm2/s/sr.
| Explorer 11 (S-15) | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1961 Apr 27 | 1416:38 | Launch by Juno II AM-19E | CC LC26B |
| T+2:58 MECO | |||
| 1419:05 | T+3:05 Jupiter sep | ||
| 1419:34 | Fairing sep | ||
| 1424:26 | T+8:26 Stage 2 burn, 495 km | ||
| Stage 3 burn | |||
| Stage 4 burn | |||
| 1424:56 | Orbit insertion, 496 km | 491 x 1799 x 28.8 | |
| Telescope cover sep? | |||
| 1961 Dec 6 | End of ops | ||
Payload:
- Cerenkov counter, 50-100 MeV (MIT/Kraushaar)