Friday, November 29, 2002

Alexis

 1993-026A


Alexis, the Array of Low Energy X-ray Imaging Sensors, was Space Test Program flight P89-1B. It was also known as ISES (Independent Space Experiment System). Alexis was developed by the Los Alamos National Laboratory (LANL) as part of its program to maintain capability to monitor nuclear explosions, and its main payload was six wide field X-ray telescopes to study the X-ray emission from the interstellar medium. A second LANL experiment, Blackbeard, was carried to study ionospheric propagation. A third experiment, the US Navy VSUME, was also carried, possibly on the Pegasus third stage.

Each of the six Alexis telescopes has a 0.128m diameter Cassegrain normal incidence multilayer spherical primary mirror with a focal length of 0.13m. The telescopes operate in the 100-200A band.

The 113 kg satellite was built by Aero Astro Inc. of Herndon, Virginia. The satellite was a 1.0m box with 4 panels.

Alexis was launched by Pegasus on 1993 Apr 25 over the Point Arguello Warning Area on the Western Test Range. During second stage burn, a solar panel was broken loose from its mounting by vibration. The satellite reached orbit but was unable to orient itself and fell silent. It was feared that the mission was a total loss, but over a month later a weak signal from the satellite was found. Repeated passes over the next few months allowed LANL scientists to regain full control of the spacecraft and orient it to get adequate solar power.

In 1999 because of low power, the Alexis telescopes were reduced to low voltage and run as a particle detector, during solar max when the background was high. In 2002, some of the telescopes were again being tested at high voltage.


Alexis 
 

DateTimeEventOrbit  

1993 Apr 25  1244  NB-52 takeoff from Edwards AFB 
 1356  Pegasus drop 13.3 km over PAWA 
 1356  Pegasus ignition 5s after drop 
 1357  Stage 1 sep T+90s 

 Stage 2 sep 
 1358 Fairing sep T+148s 
 1402 Solar panel loose T+380s 
 1405? Stage 3 burn 
 1406? Stage 3 burnout 
 1407? Stage 3 sep  100.69 740 x 833 x 70 
   100.69 749 x 844 x 70 
1993 Jun 2   First telemetry contact 
1993 Jun 30   Second comm pass 
1993 Jul 5   Full comms regained 
1993 Jul 11   Blackbeard ops begin 
1993 Jul 30    100.69 747 x 835 x 69.93 
2002 Mar   Still operating  

Aviation Week: July 15,2002

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Thursday, November 28, 2002

Aviation Week: June 17,2002

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USA-86

 1992-083A


A satellite was launched from Vandenberg aboard a Titan 4 in 1992, into an orbit which is similar to that of the KH-11 satellites. It is believed that USA 86 replaced the eighth KH-11 in the east plane 1300 LTDN SSO. The satellite was deorbited in mid-2000.


USA 86 
 

DateTimeEventOrbit  

1992 Nov 28  2134 Launch by Titan 4  V SLC4E 
 2136? T+2:00 St 1 MES 
 2146? T+2:04 SRM sep 
 2137?  T+3:59 Fairing sep
 2149? T+5:09 St 2 MES 
 2139? T+5:10 St 1 sep 
 2142? T+8:50 St 2 MECO  
 2143?  T+8:59 Titan 4 stage 2 sep  
   256 x 911 x 97.7 (UN) 
1993 Aug 12  2345?  97.37 260 x 1005 x 97.83 
1995 Aug 24    96.99 264 x 964 x 97.95 
1996 Apr 16    99.01 409 x 1012 x 97.75  
1997 Aug 1   98.97 402 x 1016 x 97.75  
1999 Sep 2    98.75 402 x 995 x 97.69 
2000 May 24    408 x 931 x 97.7 
2000 Aug 15?  Deorbited 

Sunday, November 24, 2002

The Race : the definitive story of America's battle to beat Russia to the moon

https://welib.org/md5/1a30f9eeaa467323f2657c1d8d9c92e3

Golden State, Golden Youth : The California Image in Popular Culture, 1955-1966

 https://welib.org/md5/5e397f27156cf0f10f976673f12bb8b1

Apollo 18

  1975-066A



    ASTP Crew

  • CDR Commander: Thomas P. Stafford, Brig-Gen USAF

  • CMP Command Module Pilot: Vance Brand, NASA

  • DMP Docking Module Pilot: Donald K. Slayton, NASA

Apollo CSM 111 was used for the Apollo-Soyuz Test Project in 1975.

The ASTP Apollo was launched from Kennedy Space Center on 1975 Jul 15 at 1950 and inserted into a 155 x 173 km orbit. It separated from the Saturn at 2104, and completed the transposition and docking maneuver, which in this case involved docking to the ASTP Docking Module attached to the S-IVB rocket. At 2224 the combined CSM 111/DM-2 spaceship pulled away from the rocket stage.

Apollo spent the next two days maneuvering to approach the Soyuz-19 spaceship. By 1550 on 1975 Jul 17 the two were stationkeeping and at 1609 Apollo docked with the Soyuz. The special `androgynous' docking mechanism consisted of 3 petals on the end of the DM which locked with another 3 petals on the nose of Soyuz. At 1916 the final hatch between the two spaceships was opened and Tom Stafford and Aleksei Leonov shook hands. Stafford and Slayton transferred to the Soyuz in the first of a series of crew exhanges.

The crews were back in their own ships by 2100 on Jul 18. At 1203 on Jul 19, Apollo and Soyuz undocked. Apollo moved between Soyuz and the Sun, creating an artificial solar eclipse for Soyuz, which allowed the Soviet crew to photograph the solar corona. Apollo moved back in and docked with Soyuz at 1233. This time Soyuz extended its docking mechanism simulating the active role (although Slayton aboard Apollo actually performed the docking). At 1526 on Jul 19, Apollo undocked from Soyuz again and flew around the ship shining beams of light at reflectors mounted on Soyuz, and measuring the ultraviolet spectrum of the reflection. This experiment would provide information on the composition of the thin upper atmosphere present at the spaceship's 210 km altitude. At 1842 Apollo fired its RCS jets to move away from Soyuz.

At 1947 on Jul 23 Apollo undocked from the Docking Module, leaving it in a 211 x 219 km orbit. Two SPS burns put Apollo at a stable distance of 300 km from the DM. A VHF receiver on Apollo tracked the frequency of the DM's signal, and analysis of the Doppler shift as a function of time would allow high resolution gravity mapping of the Earth's potential.

The last Apollo mission came to an end on Jul 24 in the most dangerous reentry to date in a US space mission. The SPS engine fired to deorbit the CSM at 2037, and the SM separated at 2044. During reentry, Brand failed to throw two switches which would have jettisoned the parachute cover and turned off the thrusters. The parachute cover was jettisoned manually a little late, but the thrusters continued firing. Stafford switched them off, but residual nitrogen tetroxide propellant was sucked in through the air vents. Stafford deployed the main parachute early as the astronauts began to cough and become nauseous. The parachute deployed successfully and splashdown was at 2118. The crew at once put on emergency oxygen masks - Brand had lost consciousness during the descent. CM-111 was winched aboard the USS New Orleans. It was not until the crew were on the carrier deck that Mission Control became aware that the emergency had occurred.


Apollo CSM 111 Mission Log 
 

DateTimeEventOrbit  

1975 Jul 15 1950:01 Launch from KSC LC39B 
1975 Jul 15 1952:16 S-IB inboard engine cutoff 
1975 Jul 15 1952:22 S-IB outboard engine cutoff 
1975 Jul 15 1952:22 S-IB separation  
1975 Jul 15 1952:23 S-IVB ignition 
 1952:34 Ullage rockets sep 
 1952:53 LES sep 
1975 Jul 15 1959:46 S-IVB main engine cutoff (MECO) 
1975 Jul 15 1959:56 Earth orbit insertion 155 x 173 km 
1975 Jul 15 2104:01 Separated from S-IVB  87.68 152 x 166 x 51.8 
1975 Jul 15 2128 Docked with DM-2 
1975 Jul 15 2224 Separated from S-IVB, with DM-2 attached 
1975 Jul 15 2224:01 AEM (RCS Apollo Extract Maneuver) 150 x 168 km 
1975 Jul 15 2331 ACM (SPS Apollo Circ Maneuver) 167 x 167 km 
1975 Jul 16 0128:30 NC-1 (SPS burn) 169 x 233 km 
1975 Jul 16 0420 Apollo probe removed  88.51 164 x 236 x 51.7 
1975 Jul 16 1546 DM-2 hatch open, crew entry 
1975 Jul 16 2018:00 PCM (RCS phasing correction)  168 x 226 km 
1975 Jul 17  0833   88.37 162 x 224 x 51.8 
1975 Jul 17 1251 NC-2 (SPS orbit lower)  166 x 197 km 
1975 Jul 17 1334 NCC (SPS corrective combination) 190 x 203 km 
1975 Jul 17 1412:05 NSR (SPS coelliptic sequence)  205 x 205 km 
1975 Jul 17 1516:42 TPI (Terminal Phase Initiation) 205 x 224 km x 51.8 deg 
1975 Jul 17 1530 TPM1 (RCS rendezvous burn) 
1975 Jul 17 1540 TPM2 
1975 Jul 17 1550 Stationkeeping with Soyuz-19 
1975 Jul 17 1609:09 Docked with Soyuz-19. Hard dock at 1609:30  88.96 218 x 227 x 51.8 
1975 Jul 17 1916 Hatch 3 open for crew transfer. CDR, DMP to Soyuz (CMP on Apollo) 
1975 Jul 17 2247 CDR, DMP from Soyuz to Apollo (CDR, CMP, DMP on Apollo) 
1975 Jul 18 1000 CDR, CMP from Apollo to Soyuz (DMP on Apollo) 
1975 Jul 18 1030 CDR, KDR from Soyuz to Apollo (CDR, DMP, KDR on Apollo) 
1975 Jul 18 1700? CDR, KDR to Soyuz, CMP and BI to Apollo (DMP, CMP, BI on Apollo) 
1975 Jul 18 2100 CDR to Apollo, BI to Soyuz (CDR, CMP, DMP in Apollo) 
1975 Jul 19 1203:20 CSM 111 undocked from Soyuz-19, 219 x 220 km x 51.8 
1975 Jul 19  Solar occultation experiment 
1975 Jul 19 1233:39 CSM soft dock with Soyuz-19 (hard dock 1240) 
1975 Jul 19 1526:12 CSM undocked from Soyuz-19 
1975 Jul 19 1600 Fly around Soyuz-19 
1975 Jul 19 1725 Burn for UV absorption expt 
1975 Jul 19 1842:47 SEP (RCS burn) 
1975 Jul 20  0906   88.91 216 x 225 x 51.8 
1975 Jul 21 1458 ATM (RCS Apollo Trim) 211 x 219 km 
1975 Jul 23  0042   88.76 203 x 222 x 51.8 
1975 Jul 23  1658   88.76 200 x 225 x 51.8 
1975 Jul 23 1947:00 Undocking from DM-2. 
1975 Jul 23 2022 DM-1 (SPS burn) 218 x 227 km 
1975 Jul 24 0033:42 DM-2 (SPS burn) 207 x 220 km 
1975 Jul 24  0150   88.72 200 x 221 x 51.8 
1975 Jul 24 2037:47 ADM (SPS Apollo Deorbit), 6.6 s burn 57.9m/s  
 2037:54 ADM cutoff 202 km  86.78 27 x 201 x 51.77 
1975 Jul 24 2044:09 SM-111 separation 193 km  
1975 Jul 24 2059:00 Entry interface 121 km 
1975 Jul 24 2118:24 Splashdown at 22 00 36N, 163 00 54W, 500 km west of Oahu 
  
1975 Jul 24 2159 Recovered by USS New Orleans

Saturday, November 23, 2002

Soyuz 22

 1976-093A


The reserve EPAS Soyuz 7K-TM spaceship, 11F615A12 No. 74, was refurbished and the APAS docking system replaced with an MKF-6 multispectral camera for Earth resources work. Spacecraft 74 was launched in Sep 1976 and named Soyuz-22; crew were Valeriy Bykovskiy and Vladimir Aksyonov. The Soyuz-22 spaceship entered a 65 degree inclination orbit, the first use of such an orbit for a piloted flight since the Voskhod program in 1965.


Soyuz-22 
 

DateTimeEventOrbit  

1976 Sep 15  0948:30  Launch by Soyuz-U  KB 
 0950 Blok BVGD sep 
 0953  Blok A sep 
 0957  Blok I MECO 
 0958Blok I sep
 1245   89.30 184 x 296 x 64.75 
 1830   89.59 249 x 260 x 64.75 
 2100MKF-6 cover sep 
1976 Sep 20  1630   89.50 246 x 254 x 64.76 
1976 Sep 23  0658?  Retrofire 
 0701?  DO CO 
 0712?  Modules sep 
 0717?  Entry 
 0740:47  Landed 140 km NW of Tselinograd

An Inconvenient Woman

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Seventeen: July 2002

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People like us : a season among the upper classes

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Kosmos 1281

 1981-064A


Two-tone telemetry; Medium res satellite.


Kosmos-1281 
 

DateTimeEventOrbit  

1981 Jul 7  1230 Launch by Soyuz-U  Plesetsk 
 1234 Blok-I burn 
 1238  Blok-I sep 
1981 Jul 8  90.44 198x394x72.8 
1981 Jul 10  92.30 358x416x72.8 
1981 Jul 15  92.30 358x415x72.8 
1981 Jul 21  
 0632? Deorbit 
 0642? PO sep 
 0700? Entry 
 0715? Landed 

American Gymnasts

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World Desk Reference

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Clueless

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Saturday, November 16, 2002

Gambit-3 26

  1970-031A


KH-8 26 was launched by Titan 3B Agena D from Vandenberg on 1970 Apr 15. It remained in orbit for 21 days, with a 14-day photo mission. The perigee was raised on May 1 for a solo mission of some kind.


KH-8 26 
 

DateTimeEventOrbit  

1970 Apr 15  1552  Launch by Titan 3B Agena D  V SLC4W 
 1554  Titan stage 1 sep 
 1557  Titan stage 2 sep 
 1557  Agena burn 
 1602? Agena MECO 
1970 Apr 16  0022   89.76 132 x 392 x 111.0 
1970 Apr 17  0017   89.62 128 x 382 x 111.0 
  Orbit raise 
1970 Apr 18  0441   89.79 127 x 400 x 111.0 
1970 Apr 20  0002   89.88 126 x 409 x 111.0 
1970 Apr 22  0551   89.50 128 x 370 x 111.0 
  Orbit raise 
1970 Apr 22  1949? SRV-1 fiducial 
1970 Apr 24  0704   89.88 130 x 406 x 111.0 
1970 Apr 27  0052   89.55 120 x 384 x 110.9 
  Orbit raise 
 1722   89.88 135 x 401 x 110.9 
1970 Apr 29  2030?SRV-2 recovered after 14 days 
1970 May 1  0502   89.32 128 x 353 x 110.9 
  Raise perigee 
1970 May 2  0749   89.28 141 x 335 x 110.9 
1970 May 5 0521   88.81 140 x 290 x 111.0 
1970 May 6  1145Reentered

Kosmos 909

 1977-036A



Kosmos-909 
 

DateTimeEventOrbit  

1977 May 19  1630:01 Launch by 11K65M PL 
 1638?  Stage 2 MECO-1 
 1700? Stage 2 MECO-2 
 1700? Stage 2 sep 
 1657  Perigee 
1977 May 20  117.1 990x2109x65.9 

Wednesday, November 6, 2002

GSAT-1

 2001-015A


The GSAT-1 experimental comsat is a test payload for ISRO's GSLV rocket, which is derived from PSLV. The GSLV stage 3 has a LOX/LH2 RD-56M engine. Launch was from SHAR in 2001.

GSAT was to have demoed digital audio and compressed TV from 48E; The satellite is similar to Insat-2, with a single solar array and a counterweight solar sail boom.

Control from Hassan. Mass is 1540 kg. The GSLV flight was a little underpowered, with the 12KRB stage's Isp only 454s instead of the predicted 461s.

The satellite fuel was depleted reaching near-GEO due to problems with the propulsion system. During 2001, GSAT-1 was operated by Hassan when the satellite was within view. It was operated until May 2002.

The GSLV was made up of 4 L40H boosters, the S139 stage, the L37.5 GS2 stage, and the C12 GS3 cryo stage.


GSAT-1 
 

DateTimeEventOrbit  

2001 Mar 28  1017  GSLV-D1 SOM ignition SHAR 
  SOM abort on pad 
2001 Apr 18  1013  T-4s PSOM ignite 
 1013:01  Launch  
  T+1:40 St 1 burnout 2.63 km/s 
  T+2:27 St 2 MES 
  T+2:29 GS1 sep 
  T+2:29? PSOM cutoff at 75 km 
  T+2:35 Interstage sep at 75 km 2.9km/s 
  T+4:40 Fairing sep 115 km 3.9 km/s 
  T+5:07 St 2 MECO 126 km, 5.18 km/s 
  T+5:14 St 2 sep  -4541 x 127 x 19? 
  T+5:14 St 3 MES 11:33 
  T+16:47? St 3 MECO 195 km, 10.17 km/s 
 1030:20  T+17:19 St 3 sep 
  St 3 passivation 
2001 Apr 18  1508  Apogee-1  557.93 166 x 31977 x 19.3  
 1947  Perigee-2  182 x 32140 x 19.28 (ISRO) 
2001 Apr 19  0023  LAM-1 at apogee 19:37 166 kg 3000 x 32000 x 19.3  
2001 Apr 19  1543  LAM-2 4min 75m/s  3000 x 35880 x 13.3 (ISRO) 
2001 Apr 20    724.86 4864 x 35838 x 11.5 
2001 Apr 20  2020  LAM-3 600m/s 11900 x 35830 x 5.5 
2001 Apr 23   LAM-4   
2001 Apr 25    1384.12 33800 x 35725 x 1.0 
2001 Apr 26    1384.54 33804 x 35738 x 1.0 

These Are Not My Beautiful Stories

  Summary: The chapters within are outlines for both future stories I’ve got planned (in the case that I never get around to writing them) a...