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Critical soft landing technology issues for future US space missionsA programmatic need for research and development to support parachute-based landing systems has not existed since the end of the Apollo missions in the mid-1970s. Now, a number of planned space programs require advanced landing capabilities for which the experience and technology base does not currently exist. New requirements for landing on land with controllable, gliding decelerators and for more effective impact attenuation devices justify a renewal of the landing technology development effort that existed during the Mercury, Gemini, and Apollo programs. A study was performed to evaluate the current and projected national capability in landing systems and to identify critical deficiencies in the technology base required to support the Assured Crew Return Vehicle and the Two-Way Manned Transportation System. A technology development program covering eight landing system performance issues is recommended.
Document ID
19920017641
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Macha, J. M.
(Sandia National Labs. Albuquerque, NM, United States)
Johnson, D. W.
(Sandia National Labs. Albuquerque, NM, United States)
Mcbride, D. D.
(Sandia National Labs. Albuquerque, NM, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Space Transportation
Report/Patent Number
NAS 1.26:185673
NASA-CR-185673
Report Number: NAS 1.26:185673
Report Number: NASA-CR-185673
Accession Number
92N26884
Funding Number(s)
CONTRACT_GRANT: NASA ORDER T-9317R
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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