Chang'e 1 Chang'e 1 model exhibited at UN exhibit, Vienna, 2011 Credit: © Mark Wade |
Status: Operational 2013. First Launch: 2013-12-01. Last Launch: 2013-12-01. Number: 1 . Gross mass: 3,780 kg (8,330 lb).
Ouyang Ziyuan announced the Chang'e Program (then still awaiting government approval), named after the Chinese legend about a young fairy that flew to the moon. Luan Enjie, Director of the China National Space Administration, announced China that China would finish the first phase of the Chang'e Program by 2010
Chang'e would consist of three phases or robotic spacecraft:
Ouyang said a piloted mission to the moon was not a goal for China within the next decade. This authoritatively refuted several leaks in January/February 2003 of plans for a near-term manned circumlunar flight. The orbiter was within the capability of existing Chinese boosters. The rover and lander would have to await availability of the heavy-lift CZ-5 after 2010.
Chang'e-5 Chang'e-5 Flight Test Vehicle, also called the Reentry Return Flight Test Mission. The spacecraft was launched into a 209 km x 413,000 km lunar transfer orbit. The vehicle was a precursor to the planned Chang'e-5 mission and consisted of a satellite bus similar to the Chang'e-2 lunar orbiter, topped with a reentry vehicle, a subscale version of the Shenzhou landing module. The craft made an 8-day flight to loop around the Moon and return to Earth. It passed 11,300 km from the Moon on October 27 and returned to Earth on October 31. The descent capsule separated from the main vehicle at 21:53 GMT and landed north of Hohhot at 22:42 GMT. The service module made a burn at 21:56 GMT to avoid reentry and swung past the Earth to head out towards the Earth-Moon L2 point. Stationed at L2 Lagrangian point. |
Chang'e 5 (CE 5) Null |
Chang'e 3 Credit: Manufacturer Image |
Unmanned lunar rover. Boosted into a 210 x 389 109 km x 28.5 deg lunar transfer orbit. On December 6 at 09:50 GMT the spacecraft entered a 100 km polar orbit around the Moon. The 3,800 kg wet / 1,200 kg at landing spacecraft had a descent engine and landing legs, and a variety of lunar surface science experiments. It also carried Yutu, a small 140 kg rover. On December 10 at 13:20 GMT the orbit was lowered from 100 x 100 to 15 x 100 km. At 12:59:52 GMT December 14, near perilune, the descent engine was turned on to decelerate the probe and fly it down to the surface. Chang'e-3 touched down at 13:11:18 GMT, at 19.51W 44.12N, about 43 km south of crater Laplace F in the Mare Imbrium. This was the first lunar soft landing since the USSR's Luna-24 in 1976.
Chang'e-5 Flight Test Vehicle, also called the Reentry Return Flight Test Mission. The spacecraft was launched into a 209 km x 413,000 km lunar transfer orbit. The vehicle was a precursor to the planned Chang'e-5 mission and consisted of a satellite bus similar to the Chang'e-2 lunar orbiter, topped with a reentry vehicle, a subscale version of the Shenzhou landing module. The craft made an 8-day flight to loop around the Moon and return to Earth. It passed 11,300 km from the Moon on October 27 and returned to Earth on October 31. The descent capsule separated from the main vehicle at 21:53 GMT and landed north of Hohhot at 22:42 GMT. The service module made a burn at 21:56 GMT to avoid reentry and swung past the Earth to head out towards the Earth-Moon L2 point. Stationed at L2 Lagrangian point.