LCROSS spacecraft, artist's rendering
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Mission type | Lunar impactor |
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Operator | NASA / ARC |
COSPAR ID | 2009-031B |
SATCAT no. | 35316 |
Website | LCROSS |
Mission duration | 144 days |
Spacecraft properties | |
Bus | Eagle-0 |
Manufacturer | Northrop Grumman |
Launch mass | 621 kilograms (1,369 lb) Centaur: 2,249 kilograms (4,958 lb) |
Start of mission | |
Launch date | 18 June 2009, 21:32:00 | UTC
Rocket | Atlas V 401 |
Launch site | Cape Canaveral SLC-41 |
Contractor | United Launch Alliance |
Orbital parameters | |
Reference system | Geocentric |
Regime | High Earth |
Period | 37 days |
Lunar impactor | |
Impact date | October 9, 2009, 11:37 | UTC
The Lunar Crater Observation and Sensing Satellite (LCROSS) was a robotic spacecraft operated by NASA. The mission was conceived as a low-cost means of determining the nature of hydrogen detected at the polar regions of the moon. Launched immediately after discovery of lunar water by Chandrayaan-1, the main LCROSS mission objective was to further explore the presence of water ice in a permanently shadowed crater near a lunar polar region. It was successful in confirming water in the southern lunar crater Cabeus.
It was launched together with the Lunar Reconnaissance Orbiter (LRO) on June 18, 2009, as part of the shared Lunar Precursor Robotic Program, the first American mission to the Moon in over ten years. Together, LCROSS and LRO form the vanguard of NASA's return to the Moon, and are expected to influence United States government decisions on whether or not to colonize the Moon.
LCROSS was designed to collect and relay data from the impact and debris plume resulting from the launch vehicle's spent Centaur upper stage (and data collecting Shepherding Spacecraft) striking the crater Cabeus near the south pole of the Moon.
Centaur had nominal impact mass of 2,305 kg (5,081 lb), and an impact velocity of about 9,000 km/h (5,600 mph), releasing the kinetic energy equivalent of detonating approximately 2 tons of TNT (8.86 GJ).
LCROSS suffered a malfunction on August 22, depleting half of its fuel and leaving very little fuel margin in the spacecraft.
Centaur impacted successfully on October 9, 2009, at 11:31 UTC. The Shepherding Spacecraft descended through Centaur's ejectate plume, collected and relayed data, impacting six minutes later at 11:37 UTC.