NEXT SPACEFLIGHT

Status

Success

DFH-2A 04

Launch Time
Sun Feb 04, 1990 12:27 UTC

Rocket

Long March 3
Image Credit: CASC
MASI
Status: Retired
Liftoff Thrust: 2,804 kN
Payload to LEO: 5,000 kg
Payload to GTO: 1,500 kg
Stages: 3
Strap-ons: 0
Rocket Height: 46.6 m
Fairing Diameter: 3.0 m
Fairing Height: 7.27 m

Mission Details

DFH-2A 04

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).

Payloads: 1
Total Mass: 441.0 kg
Geostationary Transfer Orbit

Location

LC-3, Xichang Satellite Launch Center, China

Stats

1990

11th orbital launch attempt

Long March 3

6th mission
1st mission of 1990
5th successful mission
5th consecutive successful mission