Mission type | Chang'e 5 precursor mission, lunar flyby and Earth reentry |
---|---|
Operator | CNSA |
COSPAR ID | 2014-065A |
SATCAT no. | 40283 |
Mission duration | 8 days, 4 hours, 42 minutes Return capsule 6 years, 1 month, 1 day Flyby/orbiter bus |
Spacecraft properties | |
Bus | DFH-3A [1] |
Manufacturer | CAST |
Launch mass | 3,300 kg [2]; (Service Module approximately 2,215 kg, return capsule under 335 kg) |
Start of mission | |
Launch date | 23 October 2014, 18:00[3][4] | UTC
Rocket | Long March 3C/G2 |
Launch site | Xichang LC-2 |
End of mission | |
Last contact | 24 November 2020, 08:50[5] Flyby/orbiter bus | UTC
Landing date | 31 October 2014, 22:42[6][7] Return capsule | UTC
Landing site | Siziwang Banner, Inner Mongolia |
Orbital parameters | |
Reference system | Geocentric |
Regime | Lunar free return |
Chang'e 5-T1 (Chinese: 嫦娥五号T1; pinyin: Cháng'é wǔhào T1) was an experimental robotic spacecraft that was launched to the Moon on 23 October 2014, by the China National Space Administration (CNSA) to conduct atmospheric re-entry tests on the capsule design planned to be used in the Chang'e 5 mission.[3][8][9] As part of the Chinese Lunar Exploration Program, Chang'e 5, launched in 2020, was a Moon sample return mission. Like its predecessors, the spacecraft is named after the Chinese Moon goddess Chang'e. The craft consisted of a return vehicle capsule and a service module orbiter.[10]
The return capsule of Chang'e 5-T1, named Xiaofei (Chinese: 小飞), meaning "little flyer" in Chinese, landed in Siziwang Banner, Inner Mongolia, on 31 October 2014, 22:42 UTC. The CE-5-T1 Service Module entered lunar orbit on 13 January 2015.[11] Its initial orbit was 200 x 5,300 km with a period of 8 hours.
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