Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
Ariane 5GS
Part of Ariane 5 Family
As Ariane 5g+ but the solid booster motors propellant load was increased by 2.43 metric tons and the case was welded, for a weight saving in dry mass of 1.9 metric tons.

Status: Active. First Launch: 2005-08-11. Last Launch: 2009-12-18. Number: 6 . Payload: 6,200 kg (13,600 lb). Thrust: 10,000.00 kN (2,248,000 lbf). Gross mass: 746,000 kg (1,644,000 lb). Height: 45.70 m (149.90 ft). Diameter: 5.40 m (17.70 ft).

3 stage vehicle consisting of 2 x Ariane EAP P240 + 1 x Ariane 5 EPC H158 + 1 x Ariane 5 EPS P2000.

LEO Payload: 6,200 kg (13,600 lb).


More at: Ariane 5GS.

Family: orbital launch vehicle. Country: France. Spacecraft: I-3K, FS-1300, Star bus, Insat 3, SPOT-5A-5B, MSG, Spacebus 4000, ATV. Projects: Galaxy, Insat, Intelsat. Launch Sites: Kourou, Kourou ELA3. Stages: Ariane 5-0 P230, Ariane 5-1 H155, Ariane 5-2. Agency: EADS.

2005 August 11 - . 08:20 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5GS.
  • Ipstar 1 - . Payload: Thaicom 4, LS-1300SX. Mass: 6,486 kg (14,299 lb). Nation: Thailand. Agency: Shinawat. Manufacturer: Palo Alto. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 28786 . COSPAR: 2005-028A. Apogee: 35,797 km (22,243 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Ariane 5GS version maiden flight. Launch delayed from July 8 and 11, 2005. Heaviest geosynchronous transfer orbit payload to date. As of 2007 Mar 11 located at 119.46E drifting at 0.009W degrees per day..

2005 October 13 - . 22:32 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5GS.
  • Galaxy 15 - . Mass: 2,033 kg (4,481 lb). Nation: USA. Agency: PanAmSat. Manufacturer: OSC. Program: Galaxy. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. USAF Sat Cat: 28884 . COSPAR: 2005-041A. Apogee: 35,796 km (22,242 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Slated to provide satellite television services to the United States market. As of 2007 Mar 10 located at 132.99W drifting at 0.009W degrees per day..
  • Syracuse 3A - . Payload: Spacebus 4000B3. Mass: 3,725 kg (8,212 lb). Nation: France. Agency: DGA. Manufacturer: Alenia. Program: Syracuse. Class: Communications. Type: Military communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 28885 . COSPAR: 2005-041B. Apogee: 35,803 km (22,246 mi). Perigee: 35,771 km (22,227 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Syracuse 3A French military communications satellite. Launch delayed from mid-February, March 15, April 14, May 31, 2005. As of 2007 Mar 10 located at 47.00E drifting at 0.010E degrees per day..

2005 December 21 - . 22:33 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5GS.
  • Insat 4A - . Mass: 3,081 kg (6,792 lb). Nation: India. Agency: ISRO. Program: Insat. Class: Communications. Type: Civilian communications satellite. Spacecraft: I-3K. USAF Sat Cat: 28911 . COSPAR: 2005-049A. Apogee: 35,798 km (22,243 mi). Perigee: 35,775 km (22,229 mi). Inclination: 0.0000 deg. Period: 1,436.10 min.

    Delayed from late July 2005. Launch delayed from August 23, October, November 14 and 30, December 8, 16 and 20. Dry mass 1385 kg. The satellite was equipped with Ku-band and C-band transponders and would join other Insats in providing telecommunications and television services to the Indian subcontinent. After three engine burns the satellite reached geostationary altitude over the Indian Ocean at 04:30 GMT on 26 December, then deployed its solar arrays. As of 2007 Mar 11 located at 83.00E drifting at 0.006W degrees per day.

  • Meteosat 9 - . Payload: MSG 2. Mass: 2,034 kg (4,484 lb). Nation: Europe. Agency: Eumetsat. Manufacturer: Alenia. Class: Earth. Type: Weather satellite. Spacecraft: MSG. USAF Sat Cat: 28912 . COSPAR: 2005-049B. Apogee: 35,793 km (22,240 mi). Perigee: 35,779 km (22,231 mi). Inclination: 1.5000 deg. Period: 1,436.10 min. Delayed from mid-February, March 15, June 2005. Meteosat Second Generation spin-stabilized weather satellite. As of 2007 Mar 10 located at 0.11W drifting at 0.024W degrees per day..

2007 October 5 - . 22:02 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5GS.
  • Optus D-2 - . Mass: 2,400 kg (5,200 lb). Nation: Australia. Agency: Optus. Manufacturer: OSC. Program: Aussat. Class: Communications. Type: Military communications satellite. Spacecraft: Star bus. USAF Sat Cat: 32252 . COSPAR: 2007-044A. Apogee: 35,889 km (22,300 mi). Perigee: 35,862 km (22,283 mi). Inclination: 0.0000 deg. Period: 1,440.70 min.

    Ku-band satellite designed to deliver television, internet, communications, and data services to Australia and New Zealand. After deployment of the two satellites, the EPS third stage made a brief burn at 23:28 GMT to make the first in-flight test the Aestus engine's restart capability. This was to be used in 2008 in the first launch of the ATV ISS resupply spacecraft.

  • Intelsat IS-11 - . Mass: 2,400 kg (5,200 lb). Nation: USA. Agency: Intelsat. Manufacturer: OSC. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. USAF Sat Cat: 32253 . COSPAR: 2007-044B. Apogee: 35,797 km (22,243 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. C and Ku-band satellite designed to provide Atlantic region communications services..

2007 December 21 - . 21:41 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5GS.
  • Rascom-QAF-1 - . Payload: Spacebus 4000B3. Mass: 4,579 kg (10,094 lb). Nation: Mauritius. Agency: RascomStarQAF. Manufacturer: Alenia. Program: Rascom. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 32387 . COSPAR: 2007-063A. Apogee: 35,796 km (22,242 mi). Perigee: 35,771 km (22,227 mi). Inclination: 0.1000 deg. Period: 1,436.00 min.

    African communications satellite with a hybrid Ku/C-band payload. Nominal owner RascomStarQAF of Port Louis, Mauritius, a subsidiary of the Regional African Satellite Communications Organization (RASCOM) based in Cote d'Ivoire. The mission and satellite control centers were located in Cameroun and Libya. The satellite was to provide voice, data and internet services throughout Africa. Ahelium leak in the propulsion system prevented use of the primary apogee motor. Reaction control motors were used instead to slowly move the satellite into geosynchronous orbit. The satellite was expected to reach its operating location, but with a shorter-than-planned operational lifetime.

  • Horizons 2 - . Payload: Star-2. Mass: 2,350 kg (5,180 lb). Nation: Bermuda. Agency: Intelsat, JSAT. Manufacturer: OSC. Program: Horizons. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. USAF Sat Cat: 32388 . COSPAR: 2007-063B. Apogee: 35,816 km (22,254 mi). Perigee: 35,815 km (22,254 mi). Inclination: 0.0000 deg. Period: 1,437.50 min.

    Launched by Horizons Satellite Holdings LLC, a joint venture of Intelsat and the Japanese JSAT company. To be placed at 74 deg W to serve United States, eastern Canada, and the Caribbean with communication services using its 16-transmitter Ku-band communications payload.


2009 December 18 - . 16:26 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5GS.
  • Helios 2B - . Mass: 4,200 kg (9,200 lb). Nation: France. Agency: Arianespace. Program: Helios. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: SPOT-5A-5B. USAF Sat Cat: 36124 . COSPAR: 2009-073A. Apogee: 680 km (420 mi). Perigee: 680 km (420 mi). Inclination: 98.0000 deg. French military surveillance satellite..


Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2017 Mark Wade - Contact
© / Conditions for Use