Saturday, October 4, 1997

Sputnik 1

   1957-001B


After the first successful flight of the R-7 (8K71) ICBM in August 1957, Korol"ev got permission to launch a satellite with it. The first satellite was called PS-1, or Prosteyshiy Sputnik 1, the ``Simplest Satellite''. The name contrasted with the original plan to launch a much larger and more sophisticated satellite known as Object D (see below). PS-1 was a simple sphere with a mass of 81 kg, and carried a temperature sensor and a radio transmitter. It was launched from Baikonur at 4 seconds past 1928 UTC on October 4, 1957. The two-stage 8K71 rocket is known in this context as the Sputnik or 8K71PS launch vehicle.

The 8K71PS, serial number M1-1PS, took off from pad 1 at NIIP-5. Almost immediately it ran into problems: the Blok-G strapon engine was slow in building up thrust, which could have triggered an automatic launch abort. A tank control system failure at T+16 seconds resulted in excessive kerosene consumption and depletion resulting in shutdown one second prior to the planned 4min 56s cutoff time. The resulting apogee was about 80 km short of the planned one.

The sphere was placed in orbit around the earth with a perigee of 215 km and an apogee of 939 km. The inclination of its orbit to the Earth's equator was 65.1 degrees. The satellite, referred to at the time in the Soviet press as the First ISZ ( Isskusstvenniy Sputnik Zemli or Artificial Earth SatelliteISZ, 1-y and in English-speaking countries as Sputnik One, transmitted its `beep beep' radio signal until October 27. Friction with the upper atmosphere caused the satellite to reenter on Jan 4, 1958. The much larger Blok-A (sometimes also called Blok-Ts, for `central stage') rocket core from the Sputnik launch vehicle was also placed in orbit, and reentered on December 1. Following the suggestion of Fred Whipple at the Smithsonian Astrophysical Observatory, the international Committee on Space Research (COSPAR) assigned the designation 1957 Alpha to the first satellite launch of year 1957; the first object to be seen by observers on the ground was the huge rocket stage, and this got the designation 1957 Alpha 1, leaving the payload itself to get the designation 1957 Alpha 2. (This system of international designations remained in force until 1963, when the Greek letters were replaced by Arabic numerals, and the numerals for individual objects were replaced by letters. Thus the 82nd launch of 1965 was 1965-82, and the pieces of that launch were labelled 82A, 82B, ... 82Z, 82AA, 82 AB, ... 82AZ, 82 BA,.., with the letters I and O excluded to avoid confusion with the numbers one and zero). Another designation system was the NORAD satellite catalog number, which is purely numerical: the rocket stage was catalog number 1, and the PS-1 satellite was catalog number 2. A nose cone covered the satellite at launch; it separated at orbit insertion and was observed as 1957 Alpha 3, but it was not given a NORAD catalog number. The final stage was observed to be magnitude -2 to +2 by visual observers, with the satellite being mag 4 to 6.

Mass of the final stage in orbit was 7790 kg according to the mass table in the 1985 Glushko encyclopedia.


PS-1 
 

DateTimeEventOrbit  

1957 Oct 4  1928:04 Launch by 8K71PS  KB LC1 
 1930:00  T+116s Blok-BVGD sep 
 1932:58  Blok-A cutoff, orbit insertion 
 1933:18? GO sep? 
 1933:18  Blok-A sep  215 x 939 x 65.1 
1957 Oct 27   End of transmissions 
1957 Dec 1   Blok A reentered over E Siberia/Alaska  
1958 Jan 4   Reentered

Friday, October 3, 1997

Le Morte D’Arthur

https://www.gutenberg.org/files/1251/1251-0.txt

https://www.gutenberg.org/files/1252/1252-0.txt



Navstar 24

 1991-047A


Navstar SVN 24 (USA 71) was launched on 1991 Jul 4. The LOSAT-X satellite was ejected from the Delta second stage into a 40 deg orbit.


Navstar 24 
 

DateTimeEventOrbit  

1991 Jul 4  0232  Launch by Delta 7925  CC LC17 
  SRM 1-9 sep 
  St 1 sep 
 0236  T+4:40? SES-1 
 0243  T+11:00? SECO-1  185 x 185 x 34? 
  T+20? SES-2 36s? 
 0252  T+20? SECO-2  180? x 400? x 34? 
 0253  T+21:03 St 2 sep 
  T+21:03 Delta/PAM-D sep   
 0254  T+22? TES 1:24 
 0255  T+23? TECO 
 0257  T+25? St 3 sep 354.53 188 x 20241 x 34.5 
 0336? SES-3 Delta burn 
 0337  T+1:05:30 LOSAT-X sep  92.70 400 x 413 x 39.97 
 0413? SES-4 Delta depletion 92.56 392 x 407 x 37.5 
1991 Jul 5  2339? Star 37XFP burn 
1991 Jul 10  2130   711.02 19765 x 20255 x 55.3 
1991 Aug 30   Operational (Plane D-1) 
1997 Feb 1   Operating at slot D-1 

Thursday, October 2, 1997

Lewis

 1997-044A


Lewis, built by TRW for NASA's SSTI (Small Spacecraft Technology Initiative) was one of the first Earth remote sensing satellites with combined high spatial and spectral resolution, having 384 spectral channels and a 30-m ground resolution in the 0.4 to 2.5 micron wavelength band. The panchromatic camera had 5-m resolution. The satellite was built by TRW/Redondo Beach and operated by TRW/Chantilly, VA, with NASA HQ having a minimal management oversight role and NASA-Stennis involved in data distribution. Mass is 403 kg full (194 kg bus, 81 kg instrument, 12 kg fuel, 116 kg u/k). Uses LEOStar/STEP bus. Size is a 1.50m hexagon 2.0m tall. The satellite was named after Meriwether Lewis (1774-1809), the American explorer. A companion satellite, Clark, was cancelled in 1998.

After delays caused partly by the failure of the first LMLV, Lewis was launched on 1997 Aug 23 into a 300 km parking orbit. Planned final orbit was 523 x 523 x 97.4. However, three days after launch the attitude control system malfunctioned, using up most of the fuel and leaving the spacecraft's solar panels pointing away from the Sun with the bus spinning at 2 revs per minute. The craft rapidly lost power and fell silent. The investigation determined that a badly designed safemode was initially to blame. A processor switch during launch was the first anomaly, and a solid state recorder failure prevented playback of launch data, complicating interpretation; and the operations team failed to declare a spacecraft emergency and call up additional resources when problems began.

The requalified LMLV was built by LMA/Denver instead of LMSC/Sunnyvale. The payload fairing is 3.9m x 2.0m. Although described as a 2-stage rocket, LMLV-1 really has three stages. Stage 2 cuts out at 190 km altitude and 900 km downrange; the OAM third stage burns from then until 320 km altitude and 12000 km downrange, imparting 620 kNs of impulse and 0.3 km/s of velocity. The LMLV OAM, built by Primex Aerospace and LMA, reached orbit with the satellite.


Lewis 
 

DateTimeEventOrbit  

1997 Aug 23  0651:01  Launch by LMLV-1  V SLC6 
 0652:30 T+1:29 Castor 120 MECO 
 0653:26 T+2:25 PLF sep 
 0653:31  T+2:30 Orbus 21D burn 
 0656:05 T+5:04 Orbus 21D MECO  -340 x 200 x 97? 
   -760? x 220? x 97 
 0656:06  T+5:05 OAM ignition 16:41 
 0712:47  T+21:46 OAM shutdown 
 0722:05  T+31:04 OAM sep 
   293 x 305 x 97 
  B-side processor in control 
 1730  SSR telemetry loss 
1997 Aug 25  1417  Loss of Earth lock attitude 
 1700? Attitude restored on command in safe mode 
 2100  Ops team off duty 
1997 Aug 26  0802  Ops team reacquire  
 0805Spacecraft in flat spin 
 1017  Commanded thruster firing 
 1100? loss of power
1997 Sep 28  0930   87.53 145 x 159 x 97.53 

1030   87.16 124 x 143 x 97.55 
 1129  Reentered 

Payload:

  • HSI Hyperspectral imager: 30-m resolution, plus 5-m panchromatic band

  • UCB Ultraviolet Cosmic Background, Diffuse EUV cosmic background radiometer, UCB

  • LEISA Linear Etalon Imaging Spectral Array 256 channel spectrometer, GSFC

Luxury Dream Homes: 154 Luxury Home Plans from Eleven Leading Designers

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Tuesday, September 30, 1997

STS-61-B (Atlantis)

 1985-109A


The second flight of Atlantis was one of the most ambitious of the 1985 missions. Three PAM-D satellite deployments were followed by a pair of spacewalks to study on-orbit assembly. A single GAS can carried experiments by Canadian high school students. The Continuous Flow Electrophoresis System and a 3M experiment for Diffuse Mixing in Organic Solids (DMOS) flew on the middeck.

After launch on 1985 Nov 27, the Mexican Morelos communications satellite was deployed only 5 hours after payload bay door opening. Morelos was a standard American-built Hughes HS-376 model spinning comsat, but because of its presence the Mexican government had been invited to send along a payload specialist, Dr. Rodolfo Neri Vela. Dr. Neri carried out a series of mid-deck experiments under the MPSE (Morelos Payload Specialist Experiments) program, mostly life sciences related.

The following day, the Aussat satellite and the Satcom K-2 satellite were deployed.

Nov 29 saw the first spacewalk of the mission. Sherwood `Woody' Spring and Jerry Ross entered the payload bay and practiced assembling and disassembling two large structures mounted on a payload bay MPESS carried. ACCESS consisted of a truss structure made of many small components, while the rival EASE was a tetrahedron consisting of a few large tubes joined by special nodes. During the EVA, Spring carried out a small device called OET from the airlock, and jettisoned it into space by hand. The OET (OEX Target, Orbiter Experiments Target) was a radar target to allow Atlantis to perform rendezvous experiments.

After a day of rest, Spring and Ross returned to the bay for EVA-2. This EVA continued the work of the first, with the EASE and ACCESS structures being reassembled and disassembled.

Atlantis returned to Earth on Dec 3, landing at Edwards AFB.


STS 61-B 
 

DateTimeEventOrbit  

1985 Nov 8   Tow to VAB  VAB/3 
1985 Nov 8   ET mate 
1985 Nov 12   Rollout  LC39A 
1985 Nov 27  0029:00  Launch from LC39A 
 0031:03  SRB sep at 44.7 km 
 0037:31  MECO at 109.9 km  88.63 63 x 350 x 28.5  
 0037:49  ET sep at 112.1 km  88.72 69 x 353 x 28.5  
 0109:24  OMS-2 (3:00) 85m/s   
 0112:25  OMS-2 CO  91.66 353 x 359 x 28.5 
 0202  PLBD open  
 0746:50  Morelos deploy 
 0802  OMS-3 (RH 13s) 3m/s  91.78 356 x 366 x 28.5 
1985 Nov 28  0120:33  Aussat deploy 
 0135  OMS-4 (RH 13s) 3m/s  91.90 364 x 370 x 28.5 
 2157:31  Satcom deploy 
 2213?  OMS-5 (LH 16s) 4m/s 92.04 368 x 381 x 28.5 
1985 Nov 29    
 2143  EVA-1 depress? 
1985 Nov 29  2145  EVA-1 (05:32)  
 2147  Hatch open  
  Spring, Ross egress 
 2200?  Begin ACCESS experiment 
 2245?  ACCESS assembled bays 1-10 
  Disassemble ACCESS 
 2311  Stow ACCESS 
 2316  at PSA 
1985 Nov 29  2330?  EASE experiment 
  Assemble/disassemble 6 times 
 2335?  Cycle 1 
 2350?  Cycle 2 
1985 Nov 30  0010?  Cycle 3 
 0030?  Cycle 4 
 0050? Cycle 5 
 0115?  Cycle 6 
 0130?  Cycle 7 
 0155?  Cycle 8 
 0215?  Stow EASE 
 0224 In airlock  
 0225  Obtain AAPS target (OET) 
1985 Nov 30  0230  OET deployed by Spring  92.06 368 x 382 x 28.5 
 0240  Moving RMS for OEX deploy obs
 0255Target stable 
 0310  Ingress procedures 
 0317  End EVA-1 
 0323  Repress 
 0816?  Stationkeep with OET (DAP test) at 10m 
 1130End OET test  92.08 368 x 383 x 28.5 
1985 Dec 1  0140?  OMS-6 (RH 49s) 15m/s  91.60 322 x 383 x 28.5 
 2022  Depress? 
 2023  Hatch open? 
1985 Dec 1  2030  EVA-2 (06:38)  
 2030?  Spring, Ross egress 
 2037  Working with MFR 
 2050?  MFR grapple 
 2100?  ACCESS configured, built 1-9 
 2129? Getting in MFR 
 2130?  EV-1 in MFR, built bay 10 
 2230?  EV-1 manipulate ACCESS from MFR 
 2240?  EV-1 off MFR 
 2245?  EV-2 on MFR 
 2250? Disassemble bay 10 
  Task work on bay 8 
 2330?  Rebuild bay 10 
 2340?  EV-2 on MFR manipulate ACCESS 
 2350?  Disassemble ACCESS 
1985 Dec 2  0000?  EV-2 off MFR 
 0010?  Stow ACCESS, unstow EASE 
 0015? EV2 on MFR 
 0030? Work with heat pipe assembly 
 0045? Build EASE 
 0100? EV2 manipulate EASE 
 0110? EV2 off MFR, EV1 on 
 0115? EV1 manipulate EASE 
 0145? EV1 in MFR disassemble EASE 
 0155? EV1 build heat pipe 
 0215?  EV1 egress MFR 
 0225?Stow EASE 
 0230?  Stow MFR 
 0230  Cleanup 
   332 x 382 x 28.5 
 0256? Ingress 
 0258  HC 
1985 Dec 2  0308  End EVA-2 

1985 Dec 3  

1716  PLBD close  91.62 322 x 384 x 28.5 
1985 Dec 3  2026:45  OMS DO (169s) 96 m/s  
 2029:34  OMS DO CO 
 2103:17  Entry  
 2133:49  Landed at RW22 EAFB 
 2134:00  NGTD 
 2135:07  Wheels stop 
1985 Dec 7  1430  SCA takeoff  EAFB 
 1750SCA landing  Kelly AFB TX 
 1932SCA takeoff 
 2215  SCA landing  KSC SLF 
1985 Dec 8  0330Tow to OPF 

Monday, September 29, 1997

Kosmos 205

  1968-016A


Zenit-2 No. 58 was launched in Mar 1968 from Plesetsk. It landed 300 km W of Tselinograd at 50 58 N 67 09 E.


Kosmos-205 
 

DateTimeEventOrbit  

1968 Mar 5  1230  Launch by 11A57  NIIP-53 LC41/1 
 1234  Blok-I burn 
 1239 Blok-I sep  89.4 199 x 292 x 65.7 
   89.4 201 x 310 x 65.7 (TASS) 
 1514  89.39 196 x 292 x 65.7 
1968 Mar 11  1709   89.24 193 x 280 x 65.6 
1968 Mar 13  0621? Deorbit 
 0621? PO sep 
 0645 Landed after 7.76d 

Parcae 1

  1976-038A


The first PARCAE satellite was launched on 30 Apr 1976. According to the NRL list, the dispenser was designated MSD (Multiple Satellite Dispenser) and operated for 41 days.


PARCAE 1 
 

DateTimeEventOrbit  

1976 Apr 30  1912 Launch by Atlas F 
 1914  T+2:04 Booster sep
 1914  T+2:24 Fairing 
 1917 T+5:21? SECO 
 1917? Atlas sep  -790? x 1050 x 63.5 
 1939? Kick stage burn 
 1941? Plume shield sep 
1976 May 12?  PL181 deployed 
1976 May 12?  PL183 deployed 
1976 May 13?   PL182 deployed 
   107.5 1092 x 1128 x 63.5 
1976 Jun 10  end of transmissions

Sunday, September 28, 1997

Hollywood Confidential

https://welib.org/md5/1bc3e1fae114b88f425a1e70ccaf4945

Aviation Week: May 4,1997

 https://welib.org/md5/25ce9de0f26a2f03c4cab22a5de74844

Kosmos 884

  1976-123A


N. Johnson reports that Kosmos-884 was destroyed on Dec 29 after recovery failed, according to Russian sources. The absence of the usual signs of such a failure makes me wonder if the claim could be an error for another satellite.


Kosmos-884 
 

DateTimeEventOrbit  

1976 Dec 17  0930 Launch by Soyuz-U  Baikonur 
 0934 Blok-I burn 
 0938 Blok-I sep 
1976 Dec 17    89.62 167 x 344 x 65.1 
1976 Dec 18   
89.33 165 x 318 x 65.0 
1976 Dec 23    89.23 164 x 307 x 65.0 
1976 Dec 24   
89.68 169 x 347 x 65.0 
1976 Dec 25    89.66 169 x 336 x 65.0 
1976 Dec 26   Change orbit 89.83 170 x 361 x 65.0 
1976 Dec 27   Change orbit 89.39 169 x 319 x 65.0 
1976 Dec 28   KDU ejected 
1976 Dec 29  0601? Deorbit 
 0611? PO sep? 
 0615? Entry? 
 0631? Landed 

May 13,2026

  https://planet4589.org/space/jsr/back/news.855.txt