DFH-2A 05

Launch Partial Failure

Liftoff Time (GMT)

12:00:00

Saturday December 28, 1991

Mission Details

Launch Notes

Satellite left in unusable orbit due to the third stage shutting down earlier than planned.

DFH-2A 05

Wiki

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

Rocket

Retired
Long March 3

Active 1984 to 2000

China Aerospace Science and Technology Corporation logo

Manufacturer

CASC

Rocket

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

Launch Site

LC-3

Xichang Satellite Launch Center, China

Fastest Turnaround

16 days 15 hours

Stats

Long March 3


8th

Mission

1st

Mission of 1991

1991


92nd

Orbital launch attempt