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The rotornet- a high-performance hypersonic decelerator for planetary entryRotating net decelerator for hypersonic reentry
Document ID
19650017025
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kyser, A. C.
(Astro Research Corp. Santa Barbara, CA, United States)
Date Acquired
August 2, 2013
Publication Date
June 1, 1965
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-247
Report Number: NASA-CR-247
Accession Number
65N26626
Funding Number(s)
CONTRACT_GRANT: NAS7-272
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROTATING DISK
HYPERSONIC REENTRY
DECELERATOR
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