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Launch Partial Failure
Liftoff Time (GMT)
12:00:00
Saturday December 28, 1991
Satellite left in unusable orbit due to the third stage shutting down earlier than planned.
China operated a constellation of three Dongfanghong DFH-2 (aka STTW = Shiyan Tongbu Tongxing Weixing) communications satellites in GEO for domestic needs. Designed, manufactured, and launched by indigenous means, the modest DFH-2 Dongfanghong DFH-2 (Dong Fang Hong - The East is Red) spacecraft were analogous to 1960's era Western GEO satellites (e.g., INTELSAT 3), although slightly heavier. With an on-orbit mass of 441 kg (compared to 433 kg for the earlier satellites), DFH-2A spacecraft were successfully placed in GEO in March 1988, December 1988, and February 1990 and positioned at 87.5 degrees E, 110.5 degrees E, and 98 degrees E, respectively. All three satellites remained on station at the end of 1994. A fourth DFH-2 was lost on 28 December 1991 when its CZ-3 upper stage failed to reignite. DFH-2A-1, 2A-2, 2A-3 were later renamed ChinaSat-1, ChinaSat-2 and ChinaSat-3, respectively. The DFH-2A was a spin-stabilized, drum-shaped satellite with a diameter of 2.1 m and a height of 3.1 m. The communications payload consisted of only two 6/4 GHz transponders with an output power of 10 W. The total electrical power capacity was assessed to be about 300 W (the first two experimental satellites were rated at 284 W).
Geostationary Transfer Orbit
1 Payload
441 kilograms
Manufacturer
CASCRocket
Height: 46.6m
Payload to Orbit
LEO: 5,000 kg
GTO: 1,500 kg
Liftoff Thrust
2,804 Kilonewtons
Fairing
Diameter: 3m
Height: 7.27m
Stages
3
8th
Mission
1st
Mission of 1991
92nd
Orbital launch attempt