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An Earth Entry Vehicle For Returning Samples From MarsThe driving requirement for design of a Mars Sample return mission is assuring containment of the returned samples. The impact of this requirement on developmental costs, mass allocation, and design approach of the Earth Entry Vehicle is significant. A simple Earth entry vehicle is described which can meet these requirements and safely transport the Mars Sample Return mission's sample through the Earth's atmosphere to a recoverable location on the surface. Detailed analysis and test are combined with probabilistic risk assessment to design this entirely passive concept that circumvents the potential failure modes of a parachute terminal descent system. The design also possesses features that mitigate other risks during the entry, descent, landing and recovery phases. The results of a full-scale drop test are summarized.
Document ID
20010059026
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Mitcheltree, R.
(NASA Langley Research Center Hampton, VA United States)
Hughes, S.
(NASA Langley Research Center Hampton, VA United States)
Dillman, R.
(NASA Langley Research Center Hampton, VA United States)
Teter, J.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AAAF Paper ARVS-102
Meeting Information
Meeting: 2nd International Symposium on Atmospheric Reentry Vehicles and Systems
Location: Arcachon
Country: France
Start Date: March 26, 2001
End Date: March 29, 2001
Sponsors: Association Aeronautique et Astronautique de France
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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