Engineering:Telstar 402
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Short description: 1994 American telecommunications satellite
Mission type | Communication |
---|---|
Operator | AT&T |
COSPAR ID | 1994-058A |
SATCAT no. | 23249 |
Mission duration | 12 years (planned) |
Spacecraft properties | |
Bus | AS-7000 |
Manufacturer | Lockheed Martin |
Launch mass | 3,485 kilograms (7,683 lb) |
Dimensions | 4.08 m × 2.22 m × 2.54 m (13.4 ft × 7.3 ft × 8.3 ft)[1] |
Power | 5000 W |
Start of mission | |
Launch date | 16 December 1994, 00:29:44 | UTC
Rocket | Ariane-42L H10+ |
Launch site | Kourou ELA-2 |
End of mission | |
Last contact | September 9, 1994 |
Decay date | November 14, 2004 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary (planned) |
Longitude | 89° W (planned) |
Perigee altitude | 292 kilometres (181 mi) |
Apogee altitude | 19,340 kilometres (12,020 mi) |
Inclination | 7.1° |
Period | 341.8 minutes |
Epoch | September 9, 1994 |
Telstar 402 was a communications satellite owned by AT&T Corporation.
Telstar 402 was successfully launched into space on September 9, 1994, by means of an Ariane-42L vehicle from the Kourou Space Center, French Guiana. It had a launch mass of 3,775 kg. The satellite was lost shortly after launch due to an explosion that occurred in the propulsion system that was caused by leakage of hot gases.[2]
References
- ↑ Telstar 402. TSE. Retrieved June 3, 2018.
- ↑ "Gas leak led to Telstar 402 explosion". Flight Global. February 28, 1995. https://www.flightglobal.com/news/articles/gas-leak-led-to-telstar-402-explosion-27771/.
External links
Original source: https://en.wikipedia.org/wiki/Telstar 402.
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