Saturday, October 25, 2014

OCO-2

 2014-035A


Replacement Orbiting Carbon Observatory to monitor atmospheric CO2 to 0.3 percent accuracy on 1000 km scales; to fly in the A-Train (leading GCOM-W1 by 185s and leading Aqua by 444.5s).

Hex cyl 2.12m long 0.94m wide, mass 454 kg wet. 45 kg of prop. Span 7.4m?


OCO 2 
 

DateTimeEventOrbit  

2014 Jul 2  0956:23 Launch by Delta 7320-10 V SLC2W 
  T+1:39 SRM 1-3 sep 
 T+4:24 MECO 
  T+4:32 St 1 sep 
  T+4:38 SES-1 
 1001:24 T+5:01 PLF sep 
 1006:43 T+10:20 SECO-1  185 x 726 x 98.1 
 1047:13 T+50:50 SES-2 
 1047:25 T+51:02 SECO-2  680 x 696 x 98.2 
 1052:38 T+56:15 OCO sep 
 1121:23 T+1:25:00 SES-3 
  T+1:25:38 SECO-3  604 x 3743 x 98.2 
 1153 T+1:56:40 SES-4 
 1153 T+1:57:31 SECO-4  2380 x 10336 x 98.2 (s) 
   253.59 2375 x 10139 x 98.2 
2014 Jul 3    98.45 687 x 690 x 98.2 
2014 Jul 10    98.54 686 x 691 x 98.2 
2014 Jul 11    98.48 682 x 689 x 98.2 
2014 Jul 25    98.48 683 x 689 x 98.2 
2014 Jul 30    98.64 693 x 693 x 98.2 
  Raise orbit 
2014 Aug 3    98.83 701 x 703 x 98.2 
2014 Aug 27    98.83 701 x 703 x 98.2 

Payload:

  • CO2/O2 spectrometer (JPL;Hamilton Sunstrand/Pomona) 135 kg; 3 bands (2 CO2, 1 O2); f/1.8 Cassegrain optics, R=20000. Bands are 1.61 mu, 2.06mu (CO2) and 0.765mu (O2).

Spaceflight: May 2014

 https://welib.org/md5/6a2d876cdbb70acd11010bbd0eb894f8

The Big Dance

https://broomheadz.com/2014/10/06/alexa-pappadopolos-fashion-1-2-1/



















Thursday, October 23, 2014

Apstar 2

 1997-062A


Apstar 2R is an FS-1300 to be launched by LM-3B. In 1999, Loral Skynet leased the entire capacity of the satellite to replace its failed Orion 3 satellite; the successor company Telesat ended the lease in 2009.

Size 31 m span, 8.6m x 9.3m deployed. Mass 3747 kg at launch.

The CZ-3B stage second burn was about 2.6km/s, requiring a mass ratio of 1.83 and the post-burn mass was around 6750 kg including payload assuming 200 kg residual fuel. This implies a propellant usage of 5600 kg.

The satellite is also known as Apstar 4 and Telstar 10.


Apstar 2
 

DateTimeEventOrbit  

1997 Oct 16  1913  Launch by CZ-3B 
  T+2:07 Booster sep 
  T+2:27 St 1 sep 
  T+3:52 Fairing 
  T+5:32 St 2 sep 
  T+5:32 St 3 MES-1 
 1923 T+10:31 MECO-1  160? x 450? x 28.5? 
 1934 T+21:21 MES-2 
 1937 T+24:20 MECO-2 
  T+26:00 Stage 3 sep 
1997 Oct 16    874.39 167 x 37656 x 24.6 
1997 Oct 18  0800? LAM1 
1997 Oct 18    1150.56 12347 x 47640 x 6.8 
1997 Oct 19  0330? LAM2 
1997 Oct 19    1707.45 34275 x 47611 x 0.1 
1997 Oct 21   LAM3? 
1997 Oct 24    1437.25 35709 x 35908 x 0.1 GEO 76.2E+0.3W 
1997 Nov 6    1436.10 35775 x 35797 x 0.1 GEO 76.5E 
1999 Oct 16    1436.10 35773 x 35799 x 0.0 GEO 76.5E 
1999   Leased by Loral Orion 
1999 Nov 17   Renamed Telstar 10 
2006 Aug 3    1436.08 35771 x 35801 x 0.0 GEO 76.5E 
2012 Oct 18    1436.10 35754 x 35819 x 0.4 GEO 76.3E 

Saturday, October 18, 2014

Integral

 2002-048A


The 3600 kg Integral (International Gamma Ray Astrophysics Lab) satellite is scheduled for launch in 2002 Apr by Proton. The joint ESA/NASA/IKI project is ESA's M2 mission. It will be placed in a 48000 x 115000 km x 51.6 deg orbit. Prime contractor is Alenia Spazio/Torino, and the service module (SVM) uses the XMM design.

The IBIS coded mask telescope has 12' resolution with 1' position accuracy. There are two detectors at IBIS' focus, ISGRI and PICsIT, with approx dE/E = 0.08, optimized at different energy ranges. The detectors are one below the other, so they both have the same field of view. ISGRI has a 2 x 4 array of 32 x 64 pixel detectors, making a total of 128 x 128 pixels. PICsIT is 64 x 64 pixels. A central 9x9 degree FOV can be fully imaged, with partial information on a 29x29 deg FOV; the actual FOV is larger due to “dithering”. The JEM-X instrument has two smaller 0.535m coded mask telescopes; the 0.7m SPI telescope and the OMC optical monitor are coaligned with JEM-X and IBIS.



Integral 
 

DateTimeEventOrbit  

2002 Oct 17  0441:00  Launch by Proton/DM2  KB LC81/23? 
 0443:06 T+2:06 St 1 sep 
 0446:35 T+5:36 St 2 sep 
 0446:42 T+5:42 GO sep 
 0450:39 T+9:39 stage 3 MECO 
 0450:50 T+9:50 st 3 sep, Parking orbit  192 x 690 x 51.6 
 0451:39 T+10:39 Adapter sep 
   93.13 198 x 656 x 51.6 (TLE) 
 0538:23 SOZ-1 burn 
 0543:21 T+1:02:21 DM2 MES-1 
 0543:23 SOZ-1 cutoff 
 0550:26 T+1:09:26 DM2 MECO-1 
 0613:26 T+1:32:26 DM2 sep  685 x 153000 x 51.6 
   688 x 152681 x 51.5 (TLE) 
2002 Oct 18  0646  Pass EL1:4 
2002 Oct 19  0002:55  Perigee-1 
2002 Oct 24  0600  PRM IPS-1 burn 84 kg prop, dV 48.1m/s  2285 x 152813 x 52.2  
2002 Oct 26?  IPS-2 burn 
2002 Oct 26   IPS-3 burn (2+3 =208 kg)  7231 x 152890 x 52 
2002 Oct 31  0954:53 AAM Apogee adjust to 72h 
2002 Nov 1    9050 x 153657 x 52.25 
2004 Jun 20    4310.07 11572 x 151132 x 67.7 
2005 Feb 20    4311.05 11879 x 150851 x 72.7 
2006 Jul 23    4306.79 12770 x 149845 x 81.3 
2014 Aug 7    4323.97 5823 x 157258 x 55.2

Thursday, October 16, 2014

Ekspress AM-3

 2005-023A


KSvyaz satellite, Launch by Proton-K/DM2 11S861 on 2005 Jun. Mass 2600 kg.

In 2014 NewSat bought capacity on the satellite following its move to 103E.


Ekspress AM3 
 

DateTimeEventOrbit  

2005 Jun 24  1941 Launch by Proton-K DM2 103L  
  T+2:06 St 1 sep 
  T+3:03 GO sep 
  T+5:33 St 2 sep 
  T+9:34 St 3 MECO 
 1950 T+9:44 St 3 sep 
 2054 T+1h13 MES-1 
 2101 T+1h20 MECO-1  231 x 35869 x 48.8  
2005 Jun 25  0211? MES-2 
 0215? MECO-2 
 0215? Blok DM2 sep 
2005 Jun 29    1431.72 35689 x 35712 x 0.0 GEO 95.6E+1.0E/d 
2005 Jul 24   Move in at 140E 
2005 Jul 27    1436.09 35779 x 35793 x 0.1 GEO 140.0E 
2006 Aug 8    1436.12 35772 x 35801 x 0.1 GEO 140.0E 
2014 May 29   Move out from 140E 1436.12 35770 x 35804 x 0.1 GEO 140E 
2014 May 30   Move in at 103E 1436.06 35782 x 35790 x 0.0 GEO 103.0E 

Monday, October 13, 2014

Daichi 2

 2014-029A


JAXA Advanced Land Observing Satellite, ALOS-2

3.4m box with 9.9m SAR and 16.5m solar panel span. 14 day repeat orbit cf ALOS-1 46? days.

Launched into 12:00LTDN SSO.


ALOS-2 
 

DateTimeEventOrbit  

2014 May 24 0305:14  Launch by H2A  Y1 
  T+2:05 SRB-A sep 
  T+4:30 Fairing sep 
  T+6:36 MECO 
  T+6:44 St 1 sep 
 0312:04 T+6:50 SEIG at 320 km 3.1 km/s 
 0320:28 T+15:14 SECO 
 0321:18 T+16:04 ALOS sep 
 0329:52 T+24:38 RISING-2 sep 
 0334:24 T+29:10 Uniform-1 sep 
 0338:34 T+33:20 Socrates sep 
 0342:44 T+37:30 SPROUT sep 
2014 May 27    97.38 630 x 635 x 97.9  
2014 Jul 19    97.33 629 x 632 x 97.9 

Payload:

  • PALSAR-2 L-band SAR 3 x 10m, 5.1 kW, 25 to 490 km swath, 1.257 GHz, 3m resolution

  • SPAISE-2 AIS receiver

  • SOFIE SOI-FPGA In-orbit Eval. Equipment to test Si-on-insulator diode focal plane array, with CIRC?

  • CIRC Compact IR Camera, MELCO. - IR imagery for wildfire detection, 8-12 mu, 200m res

Sunday, October 12, 2014

AMC-23

 2005-052A


SES Global's AMC-23 was launched on Dec 29 by an International Launch Services/Krunichev Proton-M with a Briz-M upper stage. AMC-23 is an Alcatel Alenia/Cannes Spacebus 4000 satellite which was originally built as Americom 13, then Worldsat 3, and is now to provide Ku-band and C-band multimedia and telecom services over the Pacific. The C-band payload will be partly used by the Japanese JSAT system.

Spacebus 4000C3, multimedia and telecom for POR

Mass 5035 kg.


AMC 23 
 

DateTimeEventOrbit  

2005 Dec 29  0228:40 Launch by Proton  KB LC200-39 
  T+2:03 St 1 sep 
  T+5:31 St 2 sep 
  T+5:45 GO sep 
 T+9:33 St 3 MECO 
 0237 T+9:44 St 3 sep  
   -930 x 163 x 51.4 
 0239 T+11:19 Briz MES-1 
 0247 T+19:04 MECO-1  175 x 177 x 51.5 
 0336 T+1:08:28 MES-2 
 0353 T+1:25:06 MECO-2  258 x 4999 x 50.3 
 0557 T+3:29:02 MES-3 
 0608 T+3:40:03 MECO-3 
 0608 T+3:40:53 DTB sep  314 x 15523 x 49.6 
 0610 T+3:42:07 MES-4 
 0615 T+3:47:22 MECO-4  395 x 35629 x 49.1 
 1116 T+8:48:50 MES-5 
 1123 T+8:55:55 MECO-5 
 1147 T+9:19:20 Briz sep 
2005 Dec 30    747.07 6192 x 35597 x 18.5 
2006 Jan 1 ?  LAM 
2006 Jan 3    1435.77 35759 x 35800 x 0.1  
2006 Jan 20    1436.11 35782 x 35791 x 0.0 GEO 170.0W 
2006 Feb 17    1436.08 35781 x 35791 x 0.0 GEO 172.0E 
2007 Feb   renamed GE 23 
2007 Nov 29    1436.10 35771 x 35801 x 0.1 GEO 172.0E 
2012 Jun   renamed Eutelsat 172A. 
2013 Jun 17    1436.08 35774 x 35797 x 0.0 GEO 172.0E 

Telkom 2

 2005-046B


Orbital Star 2 for PT TELKOM Tbk Indonesia to replace Palapa B4. Mass is 1975 kg launch 1217 kg BOL, 899 kg dry (elsewhere in the same Ariane press kit, 2300 kg launch is quoted). Size is 2.4 x 3.3 x 1.9m with 12.6m solar panel span. Satellite is box + 2 panels + 2 dishes.


TELKOM 2 
 

DateTimeEventOrbit  

2005 Nov 16 2346:00?  Launch by Ariane 5ECA  CSG ELA3 
  T+2:19 EAP sep  
  T+2:30 80 km 2.1 km/s 
  T+3:14 Fairing sep 117km 2.36 km/s  
  T+6:40 EPC at 165 km  
  T+7:45 162.8 5.31 km/s 
 2354:56 T+8:56 EPC MECO 
 2355:02 T+9:02 EPC sep at 161 km  -1047 x 161 km x 6.5 deg 
 2355:06 T+9:06 ESC-A MES-1 
 2359:28 T+13:28 ESC-A at 157 km  
2005 Nov 17  
 0002? EPC impact in Gulf of Guinea 4.5W 0N. 
 0010:41 T+24:41 ESC-A MECO 
 0013:24 T+27:24 Spaceway 2 sep 
 0017:34 T+31:34 SYLDA 5C sep 
 0019:22 T+33:22 Telkom 2 sep 
2005 Nov 17    631.45 278 x 35727 x 7.0 
2005 Nov 18    838.71 10401 x 35762 x 2.8 
2005 Nov 20?  LAM 
2005 Nov 21    1432.78 35656 x 35786 x 0.02 GEO 115.6E+0.8E/d 
2005 Nov 30    1436.08 35780 x 35791 x 0.0 GEO 118.0E 
2005 Dec 26    1436.09 35779 x 35793 x 0.0 GEO 118.1E 
2010 Apr 20    1436.16 35779 x 35795 x 0.0 GEO 118.0E 

Monday, October 6, 2014

Radarsat 2

 2007-061A


The Canadian Space Agency's Radarsat 2 was designed for 3-m resolution radar imaging. The imagery is sold by Radarsat International. The satellite is developed by MDA (MacDonald Dettwiler Associates), a subsidiary of Orbital Sciences which was originally to provide the FUSE medium LeoStar class bus. CSA will own the spacecraft during checkout, but ownership will then pass to MDA Geospatial Services Inc. for operations. In 2007, it was decided that Telesat would operate the satellite.



Orbit will be 798 x 798 km x 98.6 deg. Mass is 2300 kg at launch. Box with 2 panels and 1.5 x 15m SAR antenna. Size is 1.3 x 1.3 x 3.2m, with 15m span.

In Dec 1999 the contract for the bus went to Alenia (to avoid US concerns on radar resolution). Bus is a Prima (Piattaforma Riconfigurabile Italiana Multi-Applicativa) class satellite. Radar is built by Astrium/Portsmouth.

Launch by Soyuz-Fregat in 2007. Soyuz FG No Ts15000-025 and Fregat No 1015-2.


Radarsat 2 
 

DateTimeEventOrbit  

2007 Dec 14 1317:34 Launch by Soyuz-Fregat  KB LC31 
  T+1:56 Strapons sep 
  T+4:47 Blok A sep 
  T+4:49 KhO sep 
 1322:24 T+4:50 Fairing sep 
 1326:12 T+8:38 PKhO sep 
 1326:19 T+8:45 Blok I MECO 
 1326:22 T+8:48 Blok I sep  190 x 220 x 95.46 
  T+8:53 SOZ-1 
 1327:22 T+9:48 Fregat MES-1 (MDU-1) 224.6 m/s 
 1328:26 T+10:52 Fregat MECO-1  193 x 997 x 95.5 (NK) 
   196 x 1012 x 95.5 (TLE) 
  T+38:13 SOZ-2 
 1356:42 T+39:08 Fregat MES-2, 563.6 m/s  
 1359:02 T+41:28 Fregat MECO-2 
 1410:42 T+53:08 Fregat sep 
  T+3:24:30 Fregat SOZ-3 
 1642:59 T+3:25:25 Fregat deorbit MES-3 205.9 m/s  
 1643:22  T+3:25:48 MECO-3  60? x 787 x 98.7 
 1722:48  T+4:05:14 Fregat reentry 
2007 Dec 14    100.77 791 x 798 x 98.6 
2008 Jan 22    100.78 792 x 798 x 98.6 
2008 Jan 24   Orbit trim  100.70 791 x 792 x 98.6 
2008 Mar 11    100.70 791 x 792 x 98.6 
2011 Mar 31    100.70 791 x 792 x 98.6 

Payload:

  • C-band phased array radar, 3-m resolution with multipolarization, 15x1.5m

  • AOCS 6 x 1N hydrazine thrusters

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...