Wednesday, October 29, 2008

USA-184

 2006-027A


Launch by Delta IVM+(4,2) from VAFB SLC6. Uses 1666-4 PAF. 4m fairing. Launch az 154.2deg and then dog-leg.

The NROL-22 payload may be an advanced signals intelligence satellite or a data relay satellite.

The Two Wide-angle Imaging Neutral-Atom Spectrometers (TWINS) will perform stereo magnetospheric imaging. They will study the charge exchange neutral atoms over the 1-100 keV range and study large scale structure and dynamics of the magnetosphere. High energy ions hit the cold neutral hydrogen in the geocorona and accelerate the hydrogen as ENAs (Energetic Neutral Atoms). The experiment will piggyback on NRO Molniya-orbit spacecraft, either TRUMPET or SDS. The TWINS experiment is funded by the NASA Explorer program, with LANL as PI.

A NASA stereo magnetospheric imager was a secondary payload on an NRO Molniya orbit satellite launched in summer 2006 (according to the data management plan for the Explorer mission of opportunity). The NROL-22/USA-184 satellite launched in Jun 2006 is the only plausible candidate.

The Two Wide-angle Imaging Neutral-Atom Spectrometers (TWINS) will perform stereo magnetospheric imaging. They will study the charge exchange neutral atoms over the 1-100 keV range and study large scale structure and dynamics of the magnetosphere. High energy ions hit the cold neutral hydrogen in the geocorona and accelerate the hydrogen as ENAs (Energetic Neutral Atoms). The experiment will piggyback on NRO Molniya-orbit spacecraft, either TRUMPET or SDS. The TWINS experiment is funded by the NASA Explorer program, with LANL as PI.

It may also have carried the Interim Polar Adjunct communications package for the USAF. 2008 budget docs reported that two IPA packages were on orbit as of 2007 and 2006 docs indicated a planned launch in FY06.


NROL-22 
 

DateTimeEventOrbit  

2006 Jun 28  0333:00  Launch by Delta 4M+(4,2)  SLC6 
  T+1:35 SRM 1-2 off 
  T+1:55 SRM 1-2 sep 
  T+1:56 dogleg 
  T+3:55 end dogleg 
 0337:06 T+4:06 MECO 
  T+4:12 St 1 sep 
 0337:26 T+4:26 SSIC-1 
  T+4:36 Fairing sep
  T+4:37 St 2 dogleg 
  T+4:57 End dogleg 
 0347:21 T+14:21 SECO-1  193 x 2215 x 62.5 
 0413:12 T+40:12 SSIC-2 
 T+43:34 SECO-2 
  Spinup to 5 rpm 
 0427  T+54:14 St 2 sep 
   1110 x 37564 x 62.4 
   1073 x 36487 x 62.3 (UN R/B) 
   1111 x 37594 x 62.4 (UN P/L) 
2007 Jan 30   Initial TWINS A data 
2008 Feb 26    1112 x 39241 x 63.4 

Payload:

  • SIGINT payload?

  • Interim Polar Adjunct 2 (LDR Milstar package)

  • SBIRS HEO-1? Infrared payload (LM/Azusa).

  • TWINS-A Two Wide Angle Neutral Atom Spectrometers, for stereo imaging of the magnetosphere.

    • Neutral atom imager, 1-100 keV, 4 deg resolution

Sunday, October 26, 2008

Progress M-63

 2008-004A


Progress M No 363. Mass 7283 kg.


PM63 
 

DateTimeEventOrbit  

2008 Feb 5  1302:57 Launch by Soyuz-U  KB LC1 
  T+1:58 Strapons sep 
  T+2:42 GO sep 
  T+4:45 Blok A MECO 
  T+4:47 Blok A sep 
  T+4:57 KhO sep 
  T+8:45 Blok I MECO 
 1311:46 T+8:49 Blok I sep 
2008 Feb 5  
 1650:18  DV1 62.2s 25.3m/s SKD 
 1735:40  DV2 21.7s 8.5m/s SKD 
2008 Feb 6  1406:31  DV3 1.5m/s SKD 
2008 Feb 7    
 1430:13 Docking with Pirs 
2008 Apr 7  0849  Undocked 
 1150  Deorbit 

Friday, October 24, 2008

Spaceflight : the complete story from Sputnik to shuttle-- and beyond

 https://welib.org/md5/d240ea6496ea975ce3eb3db22bb02014

Raduga 2007

 2007-058A


Globus-1M comms satellite, 17F15M.

Launched by Proton-K No. 53526 with Briz-M No. 88526. Given the cover name Raduga-1M (although the KV press center called it Kosmos-2434, this name was not used in later official statements).


Raduga-1M 
 

DateTimeEventOrbit  

2007 Dec 9  0015  Launch by Proton-M  KB LC81 
  T+2:06 St 1 sep 
  T+3:03 GO sep 
  T+5:30 St 2 sep 
 0024 T+9:34 St 3 MECO 
  T+9:44 Stage 3 sep 
 0026 T+11:19 ?Briz MES-1 
 0033 T+18:55? MECO-1  173 x 173 x 51.49 
 0123? T+1:08? MES-2 
 0140? T+1:25? MECO-2  273 x 4991 x 48.8  
 0345? T+3:30? MES-3 
 0356? T+3:41? MECO-3 
 0357? T+3:42? DTB sep  316 x 17659 x 49.5 
 0358? T+3:43? MES-4 
 0403? T+3:48? MECO-4  400 x 35815 x 49.1 
   415 x 35534 x 46.49 
 0907?  T+8:52? MES-5 
 0915?  T+9:00? MECO-5   
 0917  T+9:02 Briz-M sep  1378.91 33620 x 35699 x 0.1  
2007 Dec 18    1434.87 35572 x 35952 x 0.1 GEO 79.3E+0.3E/d 
2008 Jan 14    1436.10 35775 x 35797 x 0.1 GEO 70.0E 
2008 Mar 10    1436.08 35780 x 35792 x 0.0 GEO 70.0

Thursday, October 9, 2008

Progress M-62

 2007-064A


Flight 27P, spacecraft 11F615A55 No 362. Launch mass 7136 kg including 2430 kg of cargo.


PM62 
 

DateTimeEventOrbit  

2007 Dec 23  0712:41  Launch  
  T+1:58 Strapons sep 
  T+2:42 GO sep
  T+4:45 Blok A MECO 
  T+4:47 Blok A sep 
  T+4:57 KhO sep
 0721:26 T+8:45 Blok I MECO 
 0721:30 T+8:49 Blok I sep 
 1102:07  SKD burn 41s 16.8m/s 
 1144:52  SKD burn 10.6s 4.4m/s 
2007 Dec 25  0756:21  SKD burn 2.2m/s  
2007 Dec 26  0754  Rendezvous with ISS at 400m 
 0758  Approach from 180m 
 0814:06  Docked with Pirs 
2008 Feb 4  1031:52  Undocked 
 1035  Sep-1 15s 
 1339:30  DV-1 3m/s Plazma-Progress 
2008 Feb 10  1112:59  DV-2 3m/s 
2008 Feb 11  1000:36  DV-3 3m/s 
2008 Feb 12  1022:45  DV-4 1m/s 
2008 Feb 13  0909:33  1m/s 
2008 Feb 14  0931:09 3m/s 
2008 Feb 15  0944:00  Deorbit burn 84.5m/s 140.7s 
 0946:21  Deorbit cutoff 
 1018:36  Entry  
 1023:36  Breakup 70 km 
 1029:34  Debris impact Pacific 

Tuesday, October 7, 2008

Eurasiasat 1

 2001-002A


Eurasiasat (Turksat 2) was a joint venture between Turk Telecom/Ankara and Aerospatiale. The satellite was registered with the UN by Turkey.


Eurasiasat 1 
 

DateTimeEventOrbit  

2001 Jan 10  2209 Launch by Ariane 44P V137  CSG ELA2 
  T+1:11 PAP sep 
  T+3:31 St 1 sep 
  T+3:33 St 2 TIG 
  T+4:26 Fairing 
  T+5:43 St 2 sep 
  T+5:48 St 3 MES 
 2227 T+18:54 St 3 MECO 
 2229  T+20:20 St 3 sep 
  T+20:25 St 3 avoidance 
2001 Jan 11  0730H10-3 reentered 
2001 Jan 12  792.91 8283 x 35715 x 2.9 
2001 Jan 14    1078.29 21192 x 35716 x 1.0 
2001 Jun 5    1436.06 35779 x 35792 x 0.0 GEO 42.0E 
2006 Jul 22    1436.08 35778 x 35793 x 0.04 GEO 42.0E

Saturday, October 4, 2008

“Ratsat”

 2008-048A


Falcon 1 Flight 4 carried a payload mass simulator nicknamed Ratsat. The hexagonal prism was 1.5m long and had a mass of 165 kg. The simulator was designed to remain attached to the second stage. This launch was the first to successfully reach orbit.


F4 
 

DateTimeEventOrbit  

2008 Sep 28  2315  Launch by Falcon 1  Omelek 
  T+2:37 MECO 
  T+2:42 St 1 sep 
  T+2:45 Kestrel MES 
  T+2:53 Jettison nozzle stiffeners 
  T+3:15 Fairing sep 
 2324 T+9:39 SECO  330 x 650? x 9.0 
  Coast 43.5min 
2008 Sep 29  0008 T+53m Stage 2 restart 6.8s 
  SECO-2  621 x 643 x 9.35  

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