Saturday, September 26, 2015

Panamsat 5

 1997-046A


PAS 5 was launched by ILS Proton in Aug 1997. The first HS-601HP high power satellite in the PAS system, it is an AOR satellite at 58W. The C-band Americas beam provides coverage of Latin America, the US and Canada. The satellite also provides European coverage.

Panamsat/Greenwich,CT and Hughes Galaxy/LA merged 1997 May 16.

Mass of PAS 5 is 3600 kg. PAS 5 suffered power loss in 1999, and also had trouble with its XIPS engine.

PAS 5 capacity was leased to Arabsat in 2002 as Arabsat 2C (Badr C), with the ownership remaining with Panamsat. The satellite was renamed Intelsat IS-5 in 2007.

In 2013 the satellite was moved to 50E.


PAS 5 
 

DateTimeEventOrbit  

1997 Aug 28  0033:30  Launch by Proton 387-02/DM3 No 2L  KB 
 0035:36  T+2:06 St 1 sep
 0035:42  T+2:12 Stage 2 burn 
 0039:05  T+5:35 Stage 2 sep 
 0039:14  T+5:44 GO sep 
 0043:19  T+9:49 stage 3 sep 
 0044:14  T+10:44 DM fairing sep 
 0147:50  T+1:14:20 DM-3 burn 1  
 0154:25  T+1:20:55 DM-3 MECO 
1997 Aug 28    635.87 214 x 36018 x 51.6 
  Coast for 5:05 
 0652:12  T+ 6:18:42 DM-3 burn 2 
 0714:02  T+6:40:32 DM-3 sep 
 0837  DM-3 depletion 
1997 Aug 28    804.60 8588 x 35966 x 14.6 
1997 Sep 2  2100?  LAM-1 
1997 Sep 2    973.94 16347 x 35990 x 7.0 
1997 Sep 4  2200?  LAM-2 
1997 Sep 5    1339.15 31748 x 35985 x 0.9  
1997 Sep 6  1800?  LAM-3 
1997 Sep 6    1364.24 32750 x 35985 x 0.4 
1997 Sep 8  0700? LAM-4 
1997 Sep 9    1436.15 35745 x 35830 x 0.1 GEO 57.8W 
1997 Nov 14    1436.13 35782 x 35791 x 0.0 GEO 58.0W 
1999 Oct 17    1436.12 35782 x 35792 x 0.0 GEO 58.0W 
2001 Jun 11    1436.14 35769 x 35805 x 0.1 GEO 58.1W 
2001 Jun 15   mv out 1440.77 35870 x 35885 x 0.1  
2001 Sep 9   mv in  1436.99 35787 x 35820 x 0.0 GEO 155.5W 
2002 Mar 8    1436.02 35778 x 35791 x 0.1 GEO 155.5W 
2002 Jun 2   mv out 156W 
2002 Aug 23   mv in 46W 
2002 Sep 25    1436.10 35782 x 35790 x 0.1 GEO 45.1W 
2002 Dec 5   mv out 
2002 Dec 29   mv in 25E 
2003 Jul 5    1436.12 35767 x 35806 x 0.0 GEO 26.1E 
2006 Aug 1    1436.07 35778 x 35794 x 0.0 GEO 26.1E 
2008 Oct 18   Mv out of 26E 
2009 Jan 12   Move in  1436.13 35783 x 35790 x 0.0 GEO 169.0E 
2012 Oct 16    1436.12 35775 x 35798 x 0.1 GEO 169.0E 

Sunday, September 20, 2015

Edusat

 2004-036A


Edusat (GSAT-3) launch in 2004 Sep. Launch mass 1950 kg, 820 kg dry; 1120 kg BOL.

440N ISRO LAM. 2.4 x 1.6 x 1.15m bus with 10.9m solar panel span.

Stationed at 74E with Insat 3C and Kalpana 1.

\imps{2.5}{images/04036A}


EDUSAT 
 

DateTimeEventOrbit  

2004 Sep 20  1031  Launch by GSLV-F01  SDSC 
  T+1:44 Stage 1 burnout 
  T+2:30 SOM burnout 
  T+2:30 Stage 2 burn 
  T+3:47 Fairing sep 115 km 
  T+4:48 Stage 2 burnout 
  T+5:04 Stage 3 MES 
 1047 T+16:39 Stage 3 MECO 
 1047 T+16:54 Stage 3 separation  162 x 35814 x 19.3 
2004 Sep 20  1615   630.88 162 x 35814 x 19.3 
2004 Sep 21  0218  LAM-1 49:56  804.79 8784 x 35780 x 7.0 
2004 Sep 22  0509  LAM-2 42:00  32800 x 36000 x 0.25  
2004 Sep 24  0451  LAM-3 26:15GEO61E+2.5/d 
2004 Sep 25   Deploy antenna, 3-axis stabilized 
2004 Sep 29  1643   1426.61 35590 x 35610 x 0.1 GEO 69.7E+2.4E/d 
2004 Oct 6    1436.07 35745 x 35826 x 0.1 GEO 70.8E 
2004 Oct 14   Drifting  1434.25 35748 x 35752 x 0.1 GEO 72.3E+0.5E/d 
2004 Nov 18    1436.09 35770 x 35802 x 0.0 GEO 74.0E 
2006 Aug 8    35772 x 35800 x 0.0 GEO 74.0E 
2011 Mar 10    1436.14 35757 x 35817 x 1.8 GEO 74.0E 

Ayame 1

 1979-009A


The ECS (Experimental Communications Satellite) was built by Mitsubishi and Ford to carry out communications experiments in the UHF, SHF, submillimeter and millimeter bands. It was a spin stabilized cylinder with a mass of 130 kg (260 kg at launch), 0.93 m long (1.96m with antennas) and 1.41 m diameter. After launch ECS was named Ayame (`Iris'). Planned location was 145E.

ECS was based on the ETS-2 bus. Total mass of 260 kg was 139 kg ABM, 10 kg prop, and 111 kg dry satellite. Unfortunately, contact with ECS was lost 12 seconds into the apogee motor burn. The yaw weight (a 0.7 kg mass on a 1.8m wire) meant to tumble stage 3 did not deploy from stage 3, and stage 3 collided with ECS 37s after separation.

Element sets assigned to Ayame are misidentifications until 2005, when it was found in a 12669 x 34219 km x 9.9 deg orbit.

The Star 37 final stage was cataloged 20 years later, in 1999. The decayed second stage was retrospectively cataloged in 2000 but assigned to an old catalog number originally belonging to debris from the Magsat satellite; no TLEs are available.

A debris object in near-GTO was cataloged in 2008.

N-1 Stage 2 is 5860 kg full with 4740 kg prop, 1120 kg em, 53.35 kN thrust. (ISTS10-47), or 6032 kg full 5376 kg prop, 656 kg em (ActaAst7,967). Isp 285s or 290.2s (both values in AstraAc7,967). 250s burn time or: 4706f 1015 kg empty 5722 f (ISTS11-267). I take the latter, since it's a post-flight report of an actual mission.

Mass estimate: post stage 2 burn, 1015 kg + 669 + 260 = 1944 kg; 6645 kg f; if 290s then dV = 2844 ln ( 6645 / 1944) = 3500 m/s; for stage 3 burn 260 + (669/105).


Ayame 
 

DateTimeEventOrbit  

1979 Feb 6  0846  Launch by N-I  TNSC 
  T+3:45 St 1 MECO 
  T+3:54 Stage 1 sep 
  T+3:56 Stage 2 MES 
 0850 T+4? Fairing sep
 0854 T+8:04 SECO Stage 2 cutoff, parking orbit  200 x 300 x 30.4? 
  Stage 2171 x 192 x 30.43 (SSR)  
 0911? T+25m? Star 37 burn 37s 606.8 191 x 34590 x 24.1 
 0913  Star 37 sep, failed to despin 
 0914  Star 37 collided with Ayame 
 0914  Ayame AKM and antennae damaged 
1979 Feb 6  1420? Apo 1 
 1930? Peri 1 
1979 Feb 7  0100? Apo 2 
 0530? Peri 2 
 1130? Apo 3 
 1530? Peri 3 
 2100? Apo 4 
1979 Feb 8  0150?  Peri 4 
 0800?  Apo 5 
 1130? Peri 5 
 1800? Apo 6 
 2200? Peri 6 
1979 Feb 9  0400?  Apo 7 
1979 Feb 9?  0400?  AKM burn 
  T+12s contact lost 
1979 Feb 9  0238  Misid  1500.01 36259 x 37797 x 0.5  
1979 Jul 2   Misid  1351.28 31411 x 36808 x 0.5  
1979 Nov 19   Misid  1348.81 29749 x 38371 x 0.1 
1983 Dec 9   Misid 1314.48 28448 x 38293 x 0.3 
1990 Nov 18   Misid 1312.72 29268 x 37403 x 2.0  
1993 Dec 30   Misid 1312.99 29258 x 37423 x 4.9 
2005 Jan 12   Found 854.23 12669 x 34129 x 9.9 
2013 Aug 7    854.20 12673 x 34213 x 8.0 

November 20,2006

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