Difference between revisions of "LCROSS"

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The Lunar CRater Observation and Sensing Satellite (LCROSS), was purpose built to search for [[water|H<sub>2</sub>O]] on the [[Moon]] and is to be launched as a secondary payload on [[Lunar Reconnaissance Orbiter]]. The smaller secondary payload spacecraft will travel with the Lunar Reconnaissance Orbiter (LRO) satellite to the moon on the same Atlas-Centaur EELV rocket to be launched from Cape Canaveral Air Force Station, Florida.  After launch, the 'secondary payload,' LCROSS spacecraft will arrive in the lunar vicinity independent of the LRO satellite. On the way to the moon, the LunarCROSS spacecraft's two main parts, the Shepherding Spacecraft (S-S/C) and the Centaur Upper Stage will remain coupled.
 
The Lunar CRater Observation and Sensing Satellite (LCROSS), was purpose built to search for [[water|H<sub>2</sub>O]] on the [[Moon]] and is to be launched as a secondary payload on [[Lunar Reconnaissance Orbiter]]. The smaller secondary payload spacecraft will travel with the Lunar Reconnaissance Orbiter (LRO) satellite to the moon on the same Atlas-Centaur EELV rocket to be launched from Cape Canaveral Air Force Station, Florida.  After launch, the 'secondary payload,' LCROSS spacecraft will arrive in the lunar vicinity independent of the LRO satellite. On the way to the moon, the LunarCROSS spacecraft's two main parts, the Shepherding Spacecraft (S-S/C) and the Centaur Upper Stage will remain coupled.
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[[Image:LunarImpact.jpg|left|thumb|450px|The life cycle of a lunar impact and associated time and special scales. The LCROSS measurement methods are “layered” in response to the rapidly evolving impact environment. Photo Credit: NASA]]
  
 
[[Image:LCROSSmain_lunarorbiter2.jpg|left|thumb|300px|LCROSS EDUS heading-in. Photo credit: NASA]]
 
[[Image:LCROSSmain_lunarorbiter2.jpg|left|thumb|300px|LCROSS EDUS heading-in. Photo credit: NASA]]

Revision as of 13:26, 11 August 2008

LCROSS ready to separate. Photo credit: NASA

LCROSS Lunar Crater Observation and Sensing Satellite

This article is a mission or probe stub. You can help Lunarpedia by expanding it.



Sponsor: NASA Ames Research Center

Secondary spacecraft to be ejected from NASA's Lunar Reconnaissance Orbiter

Principal Investigator: Dr. Anthony Colaprete

LCROSS page

Prime Contractor: Northrup Space Technologies of Redondo Beach, Calif.

The Lunar CRater Observation and Sensing Satellite (LCROSS), was purpose built to search for H2O on the Moon and is to be launched as a secondary payload on Lunar Reconnaissance Orbiter. The smaller secondary payload spacecraft will travel with the Lunar Reconnaissance Orbiter (LRO) satellite to the moon on the same Atlas-Centaur EELV rocket to be launched from Cape Canaveral Air Force Station, Florida. After launch, the 'secondary payload,' LCROSS spacecraft will arrive in the lunar vicinity independent of the LRO satellite. On the way to the moon, the LunarCROSS spacecraft's two main parts, the Shepherding Spacecraft (S-S/C) and the Centaur Upper Stage will remain coupled.

The life cycle of a lunar impact and associated time and special scales. The LCROSS measurement methods are “layered” in response to the rapidly evolving impact environment. Photo Credit: NASA
LCROSS EDUS heading-in. Photo credit: NASA

As the spacecraft approaches the moon's south pole, the Centaur will separate, and then will impact a crater in a polar region of the moon at 9,000 km/hr, producing an explosion equivalent to about 2,000 pounds of TNT (6.5 billion joules). The blast will jettison a plume of material out of the crater where astronomers can search the debris for signs of lunar water. The plume from the Centaur crash will develop as the S-S/C heads in towards the moon. The S-S/C will fly through the plume, and instruments on the spacecraft will analyze the cloud to look for signs of water and other compounds. Additional space and earth-based instruments also will study the huge plume, which scientists expect to be larger than 200 metric tons. The booster impact is set to occur sometime between May and August 2009, depending on launch dates. The other half of the LCROSS mission, a robotic satellite (the S-S/C), will observe the impact and then itself crash into the Moon 4 minutes later.

Most of the Moon is bone dry, of course. With virtually no atmosphere and 300° temperature swings between night and day, most of the Moon's surface is a hostile place for water. But there are a few cold, dark places where frozen water could stay put. At the lunar poles, the sun is always low on the horizon, so some crater ridges cast shadows that keep parts of the crater floors in perpetual darkness. Temperatures in the inky black shadows hover around 40° above absolute zero (-233° Celsius), cold enough for water ice to survive indefinitely.

The explosion itself will probably be hidden by the walls of the target crater. Instead, what astronomers will look for is the impact plume. An expanding cone of ejecta will rise more than 6 kilometers above the lunar surface and spread outward for about 40 km in every direction. Glistening in the sunlight, the debris is expected to shine like a 6th to 8th magnitude star—invisible to the human eye but an easy target for backyard telescopes.

LCROSS plume developing with S-SC looking outward and down. Photo credit: NASA

The LCROSS mission will help determine if there is water hidden in the permanently dark craters of one of the moon's poles. "If LCROSS's booster stage hits a patch of lunar regolith that contains at least 0.5 percent water ice, water should be detectable in the plume of ejecta," per Anthony Colaprete[1].


References