Saturday, April 14, 1984
Friday, April 13, 1984
Ariel 6
1979-047A
The final satellite in the Ariel series, UK 6, was built by Marconi-MSDS/Portsmouth for SRC, with BAe-Dyn/Bristol building the structure. Its main experiment was the Bristol university cosmic ray experiment, which was designed to detect heavy energetic nuclei. The 154 kg satellite was 1.31m long, 0.70m diameter. It was controlled from the SRC Appleton Lab's Ditton Park (Slough) site, using NASA's Winkfield ground station, and managed by AL/Slough. In summer 1980 control was moved to RAL/Chilton.
Ariel 6 was launched in Jun 1979. It operated until Feb 1982, but had problems with some of its systems, including interference from Soviet radar signals affecting the high voltage supplies, and the X-ray experiments were largely unsuccessful. The orbit passed through the SAA, creating further difficulties. Thermal control and battery charging problems also reduced observing time, and the satellite had an unexpectedly high coning angle which modulated the X-ray signals in a way that was difficult to calibrate.
The MSSL LE telescope used four grazing incidence paraboloidal mirrors each with a proportional counter. The LUX variability study used four PCs with a collimator; Ariel 5 couldn't detect varability in less than one orbit, so the Ariel 6 experiment was designed to study shorter variations.
Mass St 4 plus UK6 was 477 kg full 202 kg empty; St 4 is usually 306f 31 em, leaving 17 kg unaccounted. Size was 0.70m dia 2.74m span 1.31m high.
In late Sep 1979 the Leicester experiment on Ariel 6 detected an increase in the local particle background over the coast of South Africa, coincident with the suspected South African nuclear test.
| Ariel 6 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1979 Jun 2 | 2326 | Launch by Scout D-1 | WI |
| T+1:20 St 1 burnout | -6275 x 75 x 48.4 | ||
| T+1:26 St 1 sep | |||
| T+1:33 St 2 burn 38s | |||
| T+2:05 St 2 burnout | |||
| T+2:10 Fairing sep 152 km | -5755 x 221 x 52.2 | ||
| T+2:11 St 2 sep | |||
| T+2:11 St 3 burn | |||
| T+2:45 St 3 burnout | -4257 x 634 x 53.3 | ||
| 2336 | T+10:19 Spinup | ||
| T+10:21 St 3 sep | -4256 x 628 x 53.3 | ||
| 2336 | T+10:27 St 4 burn 34s | ||
| 2337 | T+11:01 St 4 burnout | ||
| 2338 | T+12:20 Despin (motors?) | ||
| T+12:20 Booms deploy | |||
| 2341 | T+15:20 St 4 sep | 97.2 600 x 654 x 55.0 | |
| 2349 | T+23:19 St 3 impact at 2.6N 46.6W | ||
| 1982 Feb 24 | End of operations | ||
Payload:
- Cosmic ray expt (Bristol/Fowler) Z=0 to 130; 0.74m dia scintillator
- Low energy x-ray telescope and proportional counters 0.1-2.0keV, high time resolution, MSSL/Boyd
- Variable cosmic X ray source expt, 2-50keV, Leicester/Pounds
- RAE solar cell techology expt
Kosmos 1508
1983-111A
Fifth launch to 109 min eccentric orbit.
| Kosmos-1508 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1983 Nov 11 | 1230 | Launch by 11K65M | Plesetsk |
| 1250? | Stage 2 sep | ||
| 1251 | Perigee | ||
| 1983 Nov 11 | 109.1 400x1966x82.9 | ||
Thursday, April 12, 1984
Friday, April 6, 1984
Thursday, April 5, 1984
Kosmos 1311
1981-097A
Kosmos-1311 was launched in Sep 1981; one release was carried out in Feb 1982, but the remainder were released in a campaign during Nov 1982 to Feb 1983. The satellite reentered in Aug 1983.
| Kosmos-1311 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1981 Sep 28 | 2100 | Launch by 11K65M | PL |
| 2108 | Stage 2 MECO-1 | ||
| 2130? | Stage 2 MECO-2 | ||
| 1981 Sep 28 | 94.5 463x519x83.0 | ||
| 1983 Aug 28 | reentered | ||
| No | Object | RCS | Release (approx) | Decay |
| Kosmos-1311 | 18.5 | 1983 Aug 28 | ||
| S3 rocket | 12.4 | 1983 Feb 16 | ||
| 1 | C | 1982 Feb 1 | 1982 Feb 27 | |
| 2 | D | 1982 Feb 1 | 1982 Feb 26 | |
| 3 | E | 0.16 | 1982 Nov 20 | 1982 Dec 5 |
| 4 | F | 0.17 | 1982 Nov 20 | 1982 Dec 5 |
| 5 | G | 1982 Dec 8 | 1982 Dec 17 | |
| 6 | H | 1982 Dec 8 | 1982 Dec 16 | |
| 7 | J | 1982 Dec 15 | 1982 Dec 22 | |
| 8 | K | 1982 Dec 15 | 1982 Dec 23 | |
| 9 | L | 1982 Dec 17 | 1982 Dec 24 | |
| 10 | M | 1982 Dec 17 | 1982 Dec 18 | |
| 11 | N | 1982 Dec 17 | 1982 Dec 17 | |
| 12 | P | 1982 Dec 17 | 1982 Dec 17 | |
| 13 | Q | 1982 Dec 17 | 1982 Dec 17 | |
| 14 | R | 1982 Dec 17 | 1982 Dec 31 | |
| 15 | S | 1982 Dec 25 | 1982 Dec 31 | |
| 16 | T | 1982 Dec 25 | 1982 Dec 31 | |
| 17 | U | 1983 Feb 17 | 1983 Feb 28 | |
| 18 | V | 1983 Feb 17 | 1983 Feb 28 | |
| 19 | W | 0.18 | 1983 Feb 17 | 1983 Feb 28 |
| 20 | X | 1983 Feb 17 | 1983 Feb 28 | |
| 21 | Y | 1983 Feb 17 | 1983 Feb 28 | |
| 22 | Z | 1983 Feb 17 | 1983 Feb 28 | |
| 23 | AA | 1983 Feb 20 | 1983 Feb 28 | |
| 24 | AB | 1983 Feb 20 | 1983 Feb 28 | |
Gambit-3 17
1968-099A
KH-8 17 (GAMBIT 4317) was launched on 1968 Nov 6 by Titan 3B Agena D from Vandenberg. The flight lasted 14 days.
On this mission the primary attitude control system (PACS) failed on rev 40 and the redundant RACS system, introduced on the previous mission, saved the flight.
| KH-8 17/OPS 5296 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1968 Nov 6 | 1910 | Launch by Titan 3B Agena D | V SLC4W |
| 1912? | Titan stage 1 sep | ||
| 1912 | Titan stge 2 sep | ||
| 1915 | Agena burn | ||
| 1920 | Agena MECO | ||
| 89.7 130 x 390 x 106.0 | |||
| 1968 Nov 16 | |||
| 2252? | SRV rev 163 | ||
| 1968 Nov 18 | 134 x 338 x 105.9 | ||
| 1968 Nov 19 | 2013? | 132 x 316 x 106.0 | |
| 2338? | SRV-1 ejected rev 213? | ||
| 2345? | Entry | ||
| 1968 Nov 20 | 0010? | SRV-1 recovered | |
| 1968 Nov 20 | Reentered | ||