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MCSB
 LADEE Credit: Manufacturer Image |
NASA Lunar Atmosphere and Dust Enviroment Explorer mission. It carried an ultraviolet spectrometer, a lunar dust experiment, a neutral mass spectrometer, and a laser communications experiment. An Aerojet Rocketdyne/Redmond R-4D-15 HiPAT 455N thruster, with 135 kg of propellant, was used for lunar orbit insertion and orbit maneuvers.
AKA: LADEE. Status: Operational 2013. First Launch: 2013-09-07. Last Launch: 2013-09-07. Number: 1 .
After three perigee boost maneuvers it entered lunar gravitational sphere of influence on 6 October at 18:02 GMT. The lunar orbit insertion burn at 10:57 GMT placed LADEE in a 24-hour-period 269 km x 15,772 km selenocentric orbit inclined 157 deg to the lunar equator. Two further burns, the last on 12 October at 10:40 GMT, placed the spacecraft in a 248 km x 251 km orbit. The spacecraft was lowered into an orbit with a 2 km perilune in early April 2014, and it impacted the lunar farside between 04:30 and 05:22 GMT April 18, possibly on the east rim of the crater Sundman V at 12N 93W, north of Mare Orientale.
Family: Moon,
MX.
Country: USA.
Launch Vehicles: Minotaur V.
Launch Sites: Wallops Island LA0B.
More at: 12814.
2013 September 7 - .
03:27 GMT - .
Launch Site: Wallops Island.
Launch Complex: Wallops Island LA0B.
LV Family: Peacekeeper.
Launch Vehicle: Minotaur V.
- LADEE - .
Mass: 383 kg (844 lb). Nation: USA.
Class: Moon.
Type: Lunar probe. Spacecraft Bus: MCSB.
Spacecraft: MCSB.
Decay Date: 2014-04-18 . USAF Sat Cat: 39246 . COSPAR: 2013-047A.
NASA Lunar Atmosphere and Dust Enviroment Explorer mission. It carried an ultraviolet spectrometer, a lunar dust experiment, a neutral mass spectrometer, and a laser communications experiment. An Aerojet Rocketdyne/Redmond R-4D-15 HiPAT 455N thruster, with 135 kg of propellant, was used for lunar orbit insertion and orbit maneuvers. After three perigee boost maneuvers it entered lunar gravitational sphere of influence on 6 October at 18:02 GMT. The lunar orbit insertion burn at 10:57 GMT placed LADEE in a 24-hour-period 269 km x 15,772 km selenocentric orbit inclined 157 deg to the lunar equator. Two further burns, the last on 12 October at 10:40 GMT, placed the spacecraft in a 248 km x 251 km orbit. The spacecraft was lowered into an orbit with a 2 km perilune in early April 2014, and it impacted the lunar farside between 04:30 and 05:22 GMT April 18, possibly on the east rim of the crater Sundman V at 12N 93W, north of Mare Orientale.
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