Monday, October 20, 1986

Transit O-14

 1967-092A


NNS O-14 (Oscar 14, NNS 30140) was launched in Sep 1967 and operated until Jan 1984.


NNS O-14 
 

DateTimeEventOrbit  

1967 Sep 25  0825:00  Launch by Scout A  V SLC5 
 0825  Algol burn  
 0826  Castor burn (T+1:18) 
 0827  Antares burn (T+2:02) 
  Antares burnout T+2:38? 
 0827  Coast (T+2:42) 
 0837:07 Altair burn (T+12:07) 
 0837:35? Altair burnout 
  Altair sep  
1967 Sep 25    106.8 1041 x 1116 x 89.3 
1984 Jan   end of ops
1984 Feb 1  1630  Doppler beacons off 
1984 Feb 28  1205  Doppler beacons on 
1984 Aug 20  1136  Doppler beacons on for tests 

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Saturday, October 18, 1986

Lanyard 3

 1963-032A


On the third and last LANYARD flight, mission 8003 (CORONA program flight 68), the only photos returned from the KH-6 were out of focus due to thermal design problems. This third flight came a few weeks after the test flight of the USAF's GAMBIT high resolution satellite, and the CIA program was cancelled in favour of the new Air Force system.

LANYARD/Agena orbital mass was 1604 kg. The Itek list records this flight as Mission 2006, but this is almost certainly an error. NORAD tracked a debris object, 1963-32B, in a 172 x 418 x 74.9 deg orbit (SATCAT); it reentered Aug 10. It may have been the camera door.

The index camera malfunctioned immediately and the main camera failed on orbit 23.

An NRO memo reports that the mission imaged an SR-71 Blackbird flying over Edwards.


LANYARD 3 
 

DateTimeEventOrbit  

1963 Jul 31  0000:17 Launch by TAT Agena D  V Pad 2 
 0000:27  TAT launch (NRO doc) 
 0001  Castor sep (T+1:10) 
 0002  Thor MECO (T+2:30) 
 0002  Thor VECO (T+2:39) 
 0002  Thor sep (T+2:45) 
 0002  Agena burn (T+2:50) 
 0007:17  Agena MECO (T+6:50)  90.6 168 x 467 x ? (VCR) 
 0007? Camera door ejected? 
1963 Aug 1  90.6 155 x 455 x 74.9 (SATCAT) 
1963 Aug 2  0201? SRV ejected, deorbit rev 33 
 0232  Recovered  
 0250  SRV recovered mid-air (error?) 
1963 Aug 5  1700   90.4 157 x 411 x 75.0 (RAE) 
1963 Aug 12  0520?  LANYARD/Agena reentered 

Thursday, October 16, 1986

Kosmos 287

  1969-054A


Zenit-2 No. 76 flew a 51.8 degree Baikonur mission in Jun-Jul 1969. Landing was 60 km NW of Ural'sk at 51 28 N 51 01 E.


Kosmos-287 
 

DateTimeEventOrbit  

1969 Jun 24  0650  Launch by 11A57  NIIP-5 LC31 
 0655  Blok-I burn 
 0659  Blok-I sep  89.0 190 x 268 x 51.8 (TASS) 
1969 Jun 25  0324   89.03 188 x 263 x 51.8 
1969 Jun 27  0252? Blok-I reentered 
1969 Jun 28  0956   88.92 187 x 254 x 51.8 
1969 Jul 2  0545?  Retrofire 
 0611  Landed

Tuesday, October 14, 1986

Nimbus 6

  1975-052A


Nimbus 6 carried several important experiments, including the first Earth Radiation Budget experiment and a pioneering experiment in satellite data relay and tracking, using the ATS 6 satellite. This experiment was a precursor to the use of TDRS satellites in the 1990s to relay data to Earth from the Hubble Space Telescope and other spacecraft. Launch of Nimbus 6 was at 0812 on 1975 Jun 12 using a Delta model 2910 from Vandenberg. The Delta separated at 0918 leaving Nimbus in a 1092 x 1104 km x 100.0 deg orbit, and the satellite began regular operations on Jul 14. It was decommissioned on 1983 Sep 30.


Nimbus 6 
 

DateTimeEventOrbit  

1975 Jun 12  0812:01  Launch by Delta 2910  
  T+1:25 SRM sep 
 0815:40  T+3:40 MECO 
  T+3:46 VECO 
 0815:49 T+3:48 St 1 sep 
 0815:53 T+3:53 SES-1 5:11 
 0816 T+4:26 Fairing 
 0821:05 T+9:04 SECO-1  160? x 1100 x 100.0 
 0909 T+57:05 SES-2 13s 
 0909 T+57:18 SECO-2 
 0912:38  T+1:00:37 St 2 sep  1092 x 1104 x 100.0 
 0928 T+1:16:40 SES-3 5s 
 0944:41 T+1:32:40 SES-4 8s 
 0944:49 SECO-4  1095 x 1104 x 100.0

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Friday, October 10, 1986

Kosmos 1449

 1983-024A


Two-tone telemetry; Medium res satellite


Kosmos-1449 
 

DateTimeEventOrbit  

1983 Mar 31  1050 Launch by Soyuz-U  Plesetsk 
 1054 Blok-I burn 
 1058  Blok-I sep 
1983 Mar 31    89.23 195 x 375 x 72.9 
1983 Apr 1   
92.30 358x416x72.9  
1993 Apr 10  92.26 356 x 414 x 72.9 
1983 Apr 15  
 0515? Deorbit 
 0525? PO sep 
 0543? Entry 
 0558? Landed 

Thursday, October 2, 1986

Kosmos 311

 1969-102A


DS-P1-Yu No. 27 was a Subgroup 1 mission.


Kosmos-311 
 

DateTimeEventOrbit  

1969 Nov 24  1100  Launch by 11K63  PL 
 1102 Stage 2 burn 
 1107?  Stage 2 sep 
1969 Nov 25  2130   91.99 273 x 469 x 71.04 
1970 Jan 19 1857? Stage 2 reentered 
1970 Jan?  End of operations 
1970 Mar 10  0614? Reentered 

Wednesday, October 1, 1986

Corona 135

 1969-079A


KH-4A Mission 1052 was the final KH-4A flight. It was launched on 1969 Sep 22 by Thorad Agena D from Vandenberg into an 85 degree orbit. Both of the SRVs were recovered successfully. The mission discovered new UR-100 (SS-11) silos at Pervomaysk and Derazhnaya.


KH-4A Mission 1052 
 

DateTimeEventOrbit  

1969 Sep 22  2111 Launch by Thorad SLV-2G Agena D V SLC3W 
 2112 Castor sep 
 2114 Thor sep 
 2115 Agena burn 
 2119 Agena MECO 
   88.50 152 x 252 x 85.04 (OE) 
 2302? Subsatellite ejected 
 2310? DMU 13kN burn, rev 2 
1969 Sep 22  2337   88.49 152 x 247 x 85.0 
1969 Sep 23  0700   88.62 154 x 258 x 85.0 
 1600? DMU burn 2, rev 14 
1969 Sep 24  0641   88.77 176 x 251 x 85.0 
1969 Sep 24  1832   88.73 176 x 248 x 85.0 
1969 Sep 24  0700  88.83 178 x 253 x 85.0 (RAE) 
1969 Sep 25  1217   88.69 175 x 245 x 85.0 
1969 Sep 26  0434   88.65 169 x 246 x 85.0 
1969 Sep 26   DMU burn 3, rev 56 
1969 Sep 27  0712   88.74 176 x 248 x 85.0 
1969 Sep 28  0653   88.71 177 x 244 x 85.0 
  DMU burn 4, rev 94 
1969 Sep 29  0337   88.82 176 x 255 x 85.0 
1969 Sep 29  0804   88.81 171 x 263 x 85.0 (OE) 
 2322?  SRV-1 ejected 
1969 Sep 29  2358 SRV-1 recovered 
1969 Sep 29  2252   88.77 169 x 260 x 85.0 (OE) 
1969 Sep 30   DMU burn 5, rev 133 
 1043   88.73 172 x 251 x 85.0 
 1935   88.70 168 x 252 x 85.0 
1969 Sep 30    88.7 177 x 253 x 85.0 (SSR) 
1969 Oct 1  0002   88.69 172 x 247 x 85.1 
1969 Oct 2   DMU burn 6, rev 172 
1969 Oct 2  1005   88.76 173 x 252 x 85.0 
1969 Oct 5  0909   88.73 177 x 245 x 85.0 
 2100   88.71 172 x 249 x 85.0 
  DMU burn 7, rev 221 
1969 Oct 6  2040   88.82 177 x 255 x 85.0 
1969 Oct 7 2151   88.75 170 x 257 x 85.0 (OE) 
1969 Oct 7  2220?  SRV-2 ejected 
 2257 SRV-2 recovered 
1969 Oct 8  0346   88.73 176 x 248 x 85.0 
1969 Oct 8   L/B experiment  
1969 Oct 9  0624   88.64 173 x 242 x 85.0 
1969 Oct 11  0200?  Last stable pass, rev 295  
1969 Oct 12  1230   87.56 139 x 167 x 85.0 
1969 Oct 12  1452? CORONA/Agena reentered 

Tuesday, September 30, 1986

Luna 1

 1959-012A


On the fourth launch, on Jan 2, 1959, the R-7 core worked correctly and the Blok-E got its first chance to fire. It operated successfully except for a control system malfunction. The final Blok-E stage and the E-1 No. 4 probe were placed in solar orbit, missing the Moon by 6000 km on Jan 4.

At the time there was no official name for the probe, just 'scientific instrument container of the Soviet Cosmic Rocket'. By the early 1960s it was referred to as the AMS `Luna' ( Avtomaticheskaya Mezhplanetaya Stantsiya `Luna') (known today as Luna-1), the probe was also referred to as `Mechta', reflecting the achievement of Tsiolkovskiy's `dream'. The probe carried detectors to measure the space environment; the 0.8 m diameter sphere had a mass of 205 kg (the often quoted mass of 361 kg includes a power supply attached to the final stage; possibly the sodium cloud experiment must also be subtracted). The probe stopped transmitting on Jan 5.


AMS Luna 
 

DateTimeEventOrbit  

1959 Jan 2  1641:25  Launch by 8K72  KB 
 1646? Blok-A sep 
 1646? Blok-E burn 
  Fairing sep? 
 1652:10T+11:45 Escape velocity 
1959 Jan 4  0259  Perilune 6000 km, ahead of Moon 
1959 Jan 5   End of transmissions 
1959 Jan 14   Perihelion  146M x 197M km x 1.0 deg 

Thursday, September 18, 1986

Corona 114

 1967-002A


KH-4A Mission 1038 was launched on 1967 Jan 14 by TAT Agena D from Vandenberg into an 80 degree orbit. Mission 1038-1 was completed on Jan 19 after 5 days, and Mission 1038-2 ran from Jan 19 to Jan 26 for a duration of 7 days. Both SRVs were recovered and the image quality was recorded as fair to poor, possibly due to atmospheric factors.


KH-4A Mission 1038 
 

DateTimeEventOrbit  

1967 Jan 14  2128:21 Launch by Thor SLV-2A Agena D  V SLC3W 
 2128:18  Launch (PerfER) 
 2129:17 Castor sep (T+0:56) 
 2130:51  Thor MECO (T+2:30)  
 2130:59  Thor VECO (T+2:38) 
 2131:05  Thor sep (T+2:44) 
 2131:11  Agena burn (T+2:50) 
 2136:14  Agena MECO (T+7:53)  90.18 185 x 390 x 80.00 (VCR)  
1967 Jan 14  2356   90.12 180 x 381 x 80.1 
1967 Jan 15  1327   90.08 177 x 379 x 80.1 
1967 Jan 15  1430  90.13 180 x 380 x 80.07 (RAE) 
1967 Jan 16  2230   90.05 178 x 375 x 80.08 
1967 Jan 19  2305? SRV-1 ejected rev 81 
 2331  Recovered midair (PerfR) 
1967 Jan 19  2343 SRV-1 recovered (PER) 
  26 03.0N 155 54.0W 
1967 Jan 20  1633   89.93 176 x 366 x 80.07 
1967 Jan 23  0600   89.82 175 x 356 x 80.1 
 2359   89.80 175 x 353 x 80.1 
1967 Jan 26  1620   89.68 172 x 338 x 80.1 
1967 Jan 26  2248? SRV-2 ejected rev 193 
1967 Jan 26  2327 SRV-2 recovered (PER) 
 2338  Recovered midar (PerfR) 
  23 43.0N 169 01.0W 
1967 Jan 28  0543   89.62 172 x 338 x 80.1 
1967 Feb 1  2238   88.13 146 x 217 x 80.1 
1967 Feb 2  1430?? CORONA/Agena reentered 

Tuesday, September 16, 1986

Corona 128

 1968-078A


KH-4A Mission 1048 was launched by Thorad Agena D from Vandenberg on 1968 Sep 18. Both SRVs were recovered but the forward camera failed on mission 1048-2 during pass 181D. The mission carried at least 7 DMU rockets, possibly of a modified design; the first was used as planned to achieve the nominal orbit; the next three were used to maintain orbital height; and the last three were fired retrograde and used to test out the Thiokol motors. DMU 6 and 7 were 3000 lb-s; the remaindeer were 2000 lb-s versions.


KH-4A Mission 1048 
 

DateTimeEventOrbit  

1968 Sep 18  2132  Launch by LTTAT Agena D  
 2131  Launch (PerfER) 
 2133 Castor sep 
 2135 Thor sep 
 2136 Agena burn 
 2140 Agena MECO 
 2306? Subsatellite ejected 
1968 Sep 18  2059   90.11 166 x 393 x 83.0 
  DMU burn 1 rev 4 
1968 Sep 19  1632   90.16 175 x 389 x 83.0 
1968 Sep 19   90.12 167 x 393 x 83.0 (RAE) 
1968 Sep 20  0604   90.17 182 x 383 x 83.0 
1968 Sep 22   DMU burn 2 rev 56 
1968 Sep 25  0023   90.19 177 x 390 x 83.0 
1968 Sep 27  1532   90.10 176 x 382 x 83.0 
1968 Sep 27   DMU burn 3 rev 136 
 2331? SRV-1 ejected 
1968 Sep 28  0010 SRV-1 recovered rev 145; 23 38N 169 07W 
 0015  SRV-1 recovered (PerfR) 23 38 N 169 07 W 
1968 Sep 30    90.1 178 x 391 x 83.0 (SSR) 
1968 Oct 2  2224?  SRV-2 ejected rev 224 
1968 Oct 2  2305  SRV-2 recovered 17 34N 160 49W 
1968 Oct 2  2330?  DMU burn 4 rev 225 
1968 Oct 3   DMU burn 5 rev 229, retro 6m/s 
1968 Oct 3  0951   89.49 168 x 331 x 83.1 
  DMU burn 6 rev 233, retro 9m/s 
1968 Oct 3   DMU burn 7 rev 238, retro 9m/s 
1968 Oct 5  2258   88.91 167 x 274 x 83.0 
1968 Oct 8   Reentered 

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