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PERCIVAL mission to MarsWith the downturn of the world economy, the priority of unmanned exploration of the solar system has been lowered. Instead of foregoing all missions to our neighbors in the solar system, a new philosophy of exploration mission design has evolved to insure the continued exploration of the solar system. The 'Discovery-class' design philosophy uses a low cost, limited mission, available technology spacecraft instead of the previous 'Voyager-class' design philosophy that uses a 'do-everything at any cost' spacecraft. The Percival Mission to Mars was proposed by Ares Industries as one of the new 'Discovery-class' of exploration missions. The spacecraft will be christened Percival in honor of American astronomer Percival Lowell who proposed the existence of life on Mars in the early twentieth century. The main purpose of the Percival mission to Mars is to collect and relay scientific data to Earth suitable for designing future manned and unmanned missions to Mars. The measurements and observations made by Percival will help future mission designers to choose among landing sites based on the feasibility and scientific interest of the sites. The primary measurements conducted by the Percival mission include gravity field determination, surface and atmospheric composition, sub-surface soil composition, sub-surface seismic activity, surface weather patterns, and surface imaging. These measurements will be taken from the orbiting Percival spacecraft and from surface penetrators deployed from Mars orbit. The design work for the Percival Mission to Mars was divided among four technical areas: Orbits and Propulsion System, Surface Penetrators, Gravity and Science Instruments, and Spacecraft Structure and Systems. The results for each of the technical areas is summarized and followed by a design cost analysis and recommendations for future analyses.
Document ID
19940020513
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Reed, David W.
(Texas Univ. Austin, TX, United States)
Lilley, Stewart
(Texas Univ. Austin, TX, United States)
Sirman, Melinda
(Texas Univ. Austin, TX, United States)
Bolton, Paul
(Texas Univ. Austin, TX, United States)
Elliott, Susan
(Texas Univ. Austin, TX, United States)
Hamilton, Doug
(Texas Univ. Austin, TX, United States)
Nickelson, James
(Texas Univ. Austin, TX, United States)
Shelton, Artemus
(Texas Univ. Austin, TX, United States)
Date Acquired
September 6, 2013
Publication Date
December 10, 1992
Subject Category
Astronautics (General)
Report/Patent Number
NASA-CR-195541
NAS 1.26:195541
Report Number: NASA-CR-195541
Report Number: NAS 1.26:195541
Accession Number
94N24995
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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