ChinaSat-9A

Launch Partial Failure

Liftoff Time (GMT)

16:11:00

Sunday June 18, 2017

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Mission Details

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Launch Notes

Failure in control of roll-control RCS thrusters of 3rd stage during the coast phase caused 2nd burn of 3rd stage performed in improper attitude. The payload was deployed into the wrong orbit but managed to recover by its own engines.

ChinaSat-9A

Wiki

In response to the growing demand of the regional market, Sinosat was adding a new member, Xinnuo 2 (Sinosat 2), to its fleet of satellites. With 24 Ku-band transponders on board, Sinosat-2 was the first spacecraft based on the Chinese high-power satellite platform, known as DFH-4. To ensure the time schedule and performance requirements, the telecommunication payload of the Sinosat-2 payload was imported from Alcatel. Sinosat-2 was to be delivered in the first half of 2005. Launched in October 2006, the lifetime of Sinosat-2 was to be 15 years. The new satellite will serve the need for TV broadcasting, DirectPC, and broadband multimedia systems in China as well as the neighboring areas. Reportedly the satellite failed to deploy its solar arrays after reaching geostationary orbit.

Geostationary Transfer Orbit

1 Payload

5,100 kilograms

Rocket

Active
Long March 3B/E

Active Since 2007

China Aerospace Science and Technology Corporation logo

Agency

CASC

Price

$29.15 million

Rocket

Height: 56.3m

Payload to Orbit

LEO: 11,500 kg

GTO: 5,550 kg

Liftoff Thrust

5,986 Kilonewtons

Fairing

Diameter: 4.2m

Height: 9.56m

Stages

3

Strap-ons

4

Launch Site

LC-2

Xichang Satellite Launch Center, China

Fastest Turnaround

18 days

Stats

Long March 3


93rd

Mission

3rd

Mission of 2017

2017


37th

Orbital launch attempt