Tuesday, October 29, 2013

Metop A

 2006-044A


Astrium-SAS's Metop will make up the Eumetsat Polar System (EPS) [719] and use the Spot bus from MMS-F. Mass 4175 kg launch including 316 kg of hydrazine. Launch 2005. 0930LT SSO planned. Control by Eumetsat via Kiruna. Astrium GmbH (Dornier) makes the payload module. Astrium Ltd. (MMS UK) makes the SM mechanical system.

First satellite is Metop 2, to be named Metop A after launch.

Size is 6.3 x 3.4 x 3.4 at launch, 17.6 span after deployment of the single solar array and the 2 ASCAT antenna booms each around 3m long. Shape is box + panel + 2 antennae.

By 2013 Metop A was operating as the secondary satellite with Metop B in the prime role.


Metop A launch mass breakdown 

METOP A dry 3769  
Hydrazine  316  
Adapter  90? 
Fregat prop  3724? 
Fregat dry  1000?  

Total  8900  

0930LT

17.6 x 6.7 x 5.4m mass. 11.3m span with solar array. Mass 4086 kg (BR-261) full, 3769? kg dry (or 3858 kg?) The 1666-SF adapter was used between METOP and Fregat. An interstage (PKhO) was used between Fregat and the LV.

Launch by Soyuz-2-1A No. 3 (Starsem ST16) with Fregat No. 1011 (88515?) in 2005 with new 11.4m long 4.1m dia fairing. Azimuth 354.6. Blok A and fairing drop near Perm. Blok I drop near Greenland at 81N 5W.

The 14A14 Soyuz-2-1A Fregat (Zh15000-003/1011) rocket with MetOp was transported to the launch platform PU-6.


Metop 
 

DateTimeEventOrbit  

2006 Oct 19  1628:13  Launch by Soyuz-ST (2-1A)  KB LC31 
  T+1:58 Strapon sep 
  T+4:47 Blok A MECO 
  T+4:48 Blok A sep 
  T+4:48 KhO sep 
  T+4:49 GO sep 
 1636:58 T+8:45 Blok I MECO 
 1637:02 T+8:49 Blok I sep -2280 x 230 x 98.72 
 -2299 x 221 x 98.7 (Fregat report) 
 1638:02 T+9:49 Fregat MES-1 1289.4 m/s 2771 kg 
 1645:35 T+17:22 Fregat MECO-1  170 x 820 x 98.7  
   164 x 825 x 98.7 (TLE) 
   164 x 809 x 98.7 (Fregat report) 
 1731:05 T+1:02:52 Fregat MES-2 over 140E 77S, 181.1m/s 314 kg 
 1731:57 T+1:03:44 Fregat MECO-2 over 110E 75S   
 1737:05  T+1:08 METOP sep over 85E 70S  802 x 838 x 98.7  
   101.34 818 x 826 x 98.7 (TLE) 
 1814:58 T+1:46:45 Fregat MES-3 over 15E 75N 237.7m/s 
 1815:19 T+1:47:06 Fregat MECO-3 238m/s  -31 x 824 x 98.7 
   -4 x 823 (Fregat report) 
 1852:54  Fregat reentry 100 km 
2013 Apr   Metop B continues as operational sat 

Payload:

  • ASCAT scatterometer; determines wind speed over ocean. (2 sets of 3 antennae)

  • AVHRR/3 Imager (6 bands)

  • HIRS/4 IR sounder (20 channels)

  • AMSU-A HF sounder

  • MHS Microwave humidity HF sounder (5 channel microwave radiometer)

  • SEM-2 Space environment monitor (particle spectrometer)

  • GOME 2 Vis/UV spectrometer, ozone and trace gas monitor

  • ADCS/Argos 3 Advanced Data relay

  • IASI Improved Atmospheric Sounding Interferometer, T/humidity profile; FT spectrometer in 3.4-15.5mu band.

  • SARP-3 SAR (Search and Rescue) processor

  • SARR SAR repeater, SARSAT-11

Thursday, October 24, 2013

Soyuz TMA-9 (Vostok)

 2006-040A


11F732A51 Soyuz No 219 on Soyuz 11A511U-FG No. 023.

Crew:

Mikhail Tyurin (Soyuz KDR, ISS BI-1), Capt. Mike Lopez-Alegria (Soyuz BI, ISS Cdr/SO), Anousheh Ansari (Soyuz UP).

Mass 6883 kg at docking. Launch mass 7150 kg. Total prop 880 kg. 


TMA9 
 

DateTimeEventOrbit  

2006 Sep 18  0408:40  Launch by Soyuz-FG  KB LC1 
  T+1:53 SAS sep
  T+1:58 Strapons sep 
  T+3:07 GO sep 
 0413:27 T+4:47 St 2 sep 
  T+4:57 KhO sep 
 0417:25 T+8:45 St 3 MECO 
 0417:31  Blok-I sep 
 0745:01  DV1 7.8m/s 20s 
 0815:42  DV2 12.4m/s 31s 
2006 Sep 19  0503:32  DV3 1.6m/s 5s 
2006 Sep 20  0328:48  DV 13.6m/s 
 0352:04  1.5m/s 
 0412:54  DV 30.1m/s range 115 km  
 0455:39  DV 7.4m/s range 2.9 km 
 0500:37  DV 4.7 m/s range 1.2 km 
 0503:17  DV 2.5m/s range 600m 
 0512  Begin final approach 
 0521:20  Docked with Zvezda 
2006 Oct 10  1914  HC  
 1917Undock from Zvezda 
 1934 Dock at Zarya 
 2130?  HO 
2007 Mar 29  2110HC 
 2230 Undock from Zarya 
 2254 Dock at Zvezda 
 2335HO 
2007 Apr 21  0604  HC  
 0911  Undock from Zvezda 
 0915  Sep burn  322 x 343 x 51.6 
 1142  Deorbit 4:18, 115 m/s 
 1146  Deorbit cutoff -61 x 342 x 51.6  
 1206  Modules sep 
 1209  Entry interface 
 1231:30  Landed 

Mercury-Atlas 8

 https://content.blubrry.com/spacerockethistory/SRH-2013-10-24-035.mp3

Tuesday, October 15, 2013

Shenzhou 5

 2003-045A


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The first Chinese astronaut successfully completed his mission in October 2003. Shenzhou 5 was launched by Chang Zheng 2F on Oct 15. The second stage of the CZ-2F entered a 200 x 350 km x 42.4 deg orbit together with SZ-5 and its 38-year-old pilot Yang Liwei. SZ-5 then separated from the second stage. The spacecraft consists of three modules: the descent module, the propulsion module and the orbital module. At the end of the mission, at 2135 UTC the orbital module separated to remain in orbit, and the propulsion module fired at around 2138 UTC to lower perigee into the atmosphere. The propulsion module then separated at about 2158 UTC and burnt up on reentry, leaving the descent module with its heat shield exposed to the atmosphere. SZ-5 landed at 2223 UTC in China's Nei Monggol Zizhiqu (Inner Mongolia) province, at Dorbod Xi near Siziwang 100 km N of Hohhot.

Note: As usual in Chinese culture, Yang is the astronaut's family name ("Lt-Col. Yang") in contrast to English in which the family name is placed after the personal name. Yang is the first individual to fly in space who was a Chinese citizen at the time of launch. Wang Gunjin (Taylor Wang) was born in Shanghai but was a US citizen at the time of his Shuttle flight. Two other US astronauts were born in China: Shannon Wells Lucid (Shanghai) and William Anders (Hong Kong). Yang was born near Suizhong in Liaoning province.

SZ-5 was 9.2m long 2.5m dia and mass of 7790 kg (or 7840 kg according to other sources).


SZ-5 
 

DateTimeEventOrbit  

2003 Oct 15  0100:03  Launch by CZ-2F  JQ 
  T+2:00 LES sep 
  T+2:16 SRM burnout, sep 
  T+2:38 St 1 MECO 
  T+2:39 St 1 sep, St 2 burn 
  T+3:20 Fairing sep 
  T+7:41 St 2 MECO 
 0110  T+9:43 Stage 2 VECO 
 0110  T+9:43 Stage 2 sep  89.44 190 x 302 x 42.41  
 0132  Solar panels deploy 
 0754  Orbit circularization
 1003   91.22 331 x 337 x 42.42 
 2136  OM sep over SW Africa  331 x 334 x 42.43 
 2138  Deorbit over 24S 7E  -100? x 333 x 42.4 
 2159  SM sep at 145 km 
 2204  Reentry 
 2211  Parachutes out 
 2214  Jettison heat shield 
 2223  Landed 
 2233  Recovery teams reach module 

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