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Launch Partial Failure
Liftoff Time (GMT)
17:02:00
Tuesday November 29, 1994
Satellite failed to reach the operational orbit due to a propellant leak in GTO.
The DFH-3 satellite is a medium-capacity geostationary communications satellite based on the DFH-3 Bus (three-axis-stabilized telecommunications satellite platform). The 2200 kg satellite carries 24 C-band transponders, providing six television channels and 18 communications transmission channels. It has a power supply of 2 kW and a design life of 8 years. On 29 November, DFH-3 1 was launched, entering GTO precisely as planned. Unfortunately, however, the apogee kick stage malfunctioned, causing Chinese officials to use the spacecraft's propulsion system to lift the vehicle into a sub-geosynchronous orbit where the spacecraft was declared lost.
Geostationary Transfer Orbit
1 Payload
2,200 kilograms
Manufacturer
CASCPrice
$69.70 million
Rocket
Height: 52.52m
Payload to Orbit
LEO: 8,500 kg
GTO: 2,600 kg
Liftoff Thrust
2,962 Kilonewtons
Fairing
Diameter: 3.35m
Height: 8.89m
Stages
3
11th
Mission
3rd
Mission of 1994
83rd
Orbital launch attempt