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Low-cost unmanned lunar landerTwo student groups designed unmanned landers to deliver 200 kilogram payloads to the lunar surface. Payloads could include astronomical telescopes, small lunar rovers, and experiments related to future human exploration. Requirements include the use of existing hardware where possible, use of a medium-class launch vehicle, an unobstructed view of the sky for the payload, and access to the lunar surface for the payload. The projects were modeled after Artemis, a project that the NASA Office of Exploration is pursuing with a planned first launch in 1996. The Lunar Scout design uses a Delta 2 launch vehicle with a Star 48 motor for insertion into the trans-lunar trajectory. During the transfer, the solar panels will be folded inward and the spacecraft will be powered by rechargeable nickel-cadmium batteries. The lander will use a combination of a solid rocket motor and hydrazine thrusters for the descent to the lunar surface. The solar arrays will be deployed after landing. The lander will provide power for operations to the payload during the lunar day; batteries will provide 'stay-alive' power during the lunar night. A horn antenna on the lander will provide communications between the payload and the earth.
Document ID
19940021206
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Daniel, Walter K.
(Naval Academy Annapolis, MD, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Publication Information
Publication: USRA, Proceedings of the 8th Annual Summer Conference: NASA(USRA Advanced Design Program
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
94N25699
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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