China's first satellite was successfully launched into orbit in April 1970, and China has since developed a dozen or so geosynchronous orbit communications satellites.
Four types of geo-synchronous orbit communications satellite have so far been developed, namely the successful DFH-2, DFH-2A, DFH-3 and DFH-4. DFH-2 and DFH-2A satellites are spin-stabilised, while DFH-3 and DFH-4 are 3-axis stabilised.
The DFH-4 satellite is a Chinese third-generation communications satellite characterised by its high power, heavy payload capacity and extended service life. With a design life span of 15 years, it can accommodate various C, Ka, Ku and S band transponders for communications, broadcast and DTH satellite services.
The technical parameters for the DFH series of communications satellites are listed below:
DFH-2 | DFH-2A | DFH-3 | DFH-4 | |
Satellite Lift-off Mass (kg) | 920 | 1044 | 2320 | 5200 |
Power (kw) | —— | —— | 1.7 | 10.5 (EOL) |
In-Orbit Life Span (years) | 3 | >4 | >8 | 15 |
Transponders | C | C | C/Ku | S/C/Ka/Ku |
Number of Transponders | 2 | 4 | 24 | 54 |
Stabilisation Mode | Spin stabilised | Spin stabilised | 3-axis | 3-axis |
As of May 15, 2009, China Great Wall Industry Corporation (CGWIC) has signed four contracts for DFH-4 satellite in-orbit delivery. The signature in December 2004 of the contract for the in-orbit delivery of the NigComSat-1 satellite marked a major milestone for the emergence of Chinese satellites on the world commercial satellite market. The NigComSat-1 satellite was delivered in July 2007, and VeneSat-1 was subsequently delivered to Venezuela in December 2008.
The third and fourth DFH-4 communications satellites are currently under development for our international clients.