LCROSS spacecraft, artist's rendering |
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| Operator | NASA/Ames Research Center |
|---|---|
| Mission type | Impactor |
| Launch date | 2009-06-18 21:32:00 UTC |
| Launch vehicle | Atlas V 401 |
| Launch site | Cape Canaveral SLC-41 |
| Mission duration | June 18, 2009 – October 9, 2009 Elapsed: 2 years, 8 months and 8 days |
| COSPAR ID | 2009-031B |
| Homepage | http://www.nasa.gov/LCROSS |
| Mass | LCROSS Shepherding Spacecraft: 621 kg (1,369 lb) (min.); Centaur at impact: 2,249 kg (4,958 lb) (min.)[1] |
| Orbital elements | |
| Regime | Highly elliptical |
| Orbital period | 37 days |
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.[2] The main LCROSS mission objective was to explore the presence of water ice in a permanently shadowed crater near a lunar polar region.[3] It was successful in discovering water in the southern lunar crater Cabeus.[4]
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.[5]
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 10,000 km/h (6,200 mph).[6][7]
LCROSS suffered a malfunction on August 22, depleting half of its fuel and leaving very little fuel margin in the spacecraft.[8]
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.[9]
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LCROSS was a fast-track, low-cost companion mission to the LRO. The LCROSS payload was added after NASA moved the LRO from the Delta II to a larger launch vehicle. It was chosen from 19 other proposals.[10] LCROSS's mission was dedicated to late American broadcaster Walter Cronkite.[6]
LCROSS launched with the LRO aboard an Atlas V rocket from Cape Canaveral, Florida, on June 18, 2009, at 21:32 UTC (17:32 EDT). On June 23, four and a half days after launch, LCROSS and its attached Centaur booster rocket successfully completed a lunar swingby and entered into polar Earth orbit with a period of 37 days, positioning LCROSS for impact on a lunar pole.[11][12]
Early in the morning on August 22, 2009, LCROSS ground controllers discovered an anomaly caused by a sensor problem, which had resulted in the spacecraft burning through 140 kilograms (309 pounds) of fuel, more than half of the fuel remaining at the time. According to Dan Andrews, the LCROSS project manager, "Our estimates now are if we pretty much baseline the mission, meaning just accomplish the things that we have to [do] to get the job done with full mission success, we're still in the black on propellant, but not by a lot."[8]
Lunar impacts, after approximately three orbits, occurred on October 9, 2009, with the Centaur crashing into the Moon at 11:31 UTC and the Shepherding Spacecraft following a few minutes later.[13] The mission team initially announced that Cabeus A would be the target crater for the LCROSS dual impacts,[14] but later refined the target to be the larger, main Cabeus crater.[15]
On its final approach to the Moon, the Shepherding Spacecraft and Centaur separated October 9, 2009, at 01:50 UTC.[16] The Centaur upper stage acted as a heavy impactor to create a debris plume that rose above the lunar surface. Following four minutes after impact of the Centaur upper stage, the Shepherding Spacecraft flew through this debris plume, collecting and relaying data back to Earth before it struck the lunar surface to produce a second debris plume. The impact velocity was projected to be 9,000 km/h (5,600 mph).[17] The actual impact was later calculated to have been over 10,000 km/h (6,200 mph).[6]
The Centaur impact was expected to excavate more than 350 metric tons (390 short tons) of lunar material and create a crater about 20 m (65 ft) in diameter to a depth of about 4 m (13 ft). The Shepherding Spacecraft impact was projected to excavate an estimated 150 metric tons (170 short tons) and create a crater 14 m (46 ft) in diameter to a depth of about 2 m (6 ft). Most of the material in the Centaur debris plume was expected to remain at (lunar) altitudes below 10 km (6 mi).[1]
It was hoped that spectral analysis of the resulting impact plume would help to confirm preliminary findings by the Clementine and Lunar Prospector missions which hinted that there may be water ice in the permanently shadowed regions. Mission scientists expected that the Centaur impact plume would be visible through amateur-class telescopes with apertures as small as 25 to 30 cm (10 to 12 inches).[14] But no plume was observed by such amateur telescopes. Even world class telescopes such as the Hale telescope, equipped with adaptive optics, did not detect the plume. The plume may have still occurred but at a small scale not detectable from earth. Both impacts were also monitored by Earth-based observatories and by orbital assets, such as the Hubble Space Telescope.
Whether or not LCROSS would find water had been stated to be influential in whether or not the United States government pursues creating a Moon base.[18] On November 13, 2009, NASA confirmed that water was detected after the Centaur impacted the crater.[4]
The LCROSS mission took advantage of the structural capabilities of the Evolved Expendable Launch Vehicle (EELV) Secondary Payload Adapter (ESPA) ring[19] used to attach LRO to the Centaur upper stage rocket. Mounted on the outside of the ESPA were six panels that hold the spacecraft's science payload, command and control systems, communications equipment, batteries, and solar panels. A small monopropellant propulsion system was mounted inside of the ring. Also attached were two S Band omnidirectional antennas and two medium-gain antennas. The mission's strict schedule, mass, and budget constraints posed difficult challenges to engineering teams from NASA Ames Research Center (ARC) and Northrop Grumman. Their creative thinking led to a unique use of the ESPA ring and innovative sourcing of other spacecraft components. Usually, the ESPA ring is used as a platform to hold six small deployable satellites; for LCROSS, it became the backbone of the satellite, a first for the ring. LCROSS also took advantage of commercially available instruments and used many of the already-flight-verified components used on LRO.
LCROSS is managed by NASA's ARC and was built by Northrop Grumman. The LCROSS preliminary design review was completed on September 8, 2006. The LCROSS mission passed its Mission Confirmation Review on February 2, 2007,[20] and its Critical Design Review on February 22, 2007.[21] After assembly and testing at Ames, the instrument payload, provided by Ecliptic Enterprises Corporation,[22] was shipped to Northrop Grumman on January 14, 2008, for integration with the spacecraft.[23] LCROSS passed its review on February 12, 2009.
The LCROSS science instrument payload, provided by NASA's ARC, consisted of a total of nine instruments: one visible, two near infrared, and two mid-infrared cameras; one visible and two near-infrared spectrometers; and a photometer. A data handling unit (DHU) collected the information from each instrument for transmission back to LCROSS Mission Control. Because of the schedule and budget constraints, LCROSS took advantage of rugged, commercially available components. The individual instruments went through a rigorous testing cycle that simulated launch and flight conditions, identifying design weaknesses and necessary modifications for use in space, at which point the manufacturers were allowed to modify their designs.[1]
The impact was not as visually prominent as had been anticipated. Project manager Dan Andrews believed that this was due to pre-crash simulations that exaggerated the plume's prominence. Because of data bandwidth issues, the exposures were kept short, which made the plume difficult to see in the images in the visible spectra. This resulted in the need for image processing to increase clarity. The infrared camera also captured a thermal signature of the booster's impact.[24]
On 13 November 2009, NASA reported that multiple lines of evidence show water was present in both the high-angle vapor plume and the ejecta curtain created by the LCROSS Centaur impact. As of November 2009[update], the concentration and distribution of water and other substances required more analysis.[4] Additional confirmation came from an emission in the ultraviolet spectrum that was attributed to hydroxyl fragments, a product from the break-up of water by sunlight.[4] Analysis of the spectra indicate that a reasonable estimate of the concentration of water in the frozen regolith is on the order of one percent.[25] Evidence from other missions suggests that this may have been a relatively dry spot, as thick deposits of relatively pure ice appear to present themselves in other craters.[26] A later, more definitive, analysis found the concentration of water to be "5.6 ± 2.9% by mass."[27]
| LCROSS lunar swingby photos (June 23, 2009)[28] | |||||||||
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| LCROSS Centaur separation photos (Impact - 9hrs 40min, October 9, 2009)[29] | |||||||||
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| Centaur/LCROSS impact photos (11:31 UTC October 9, 2009)[30] | |||||||||
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LCROSS has received numerous awards for its technical, managerial, and scientific accomplishments.
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