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Deployment and performance characteristics of 5-foot diameter /1.5 m/ attached inflatable decelerators from Mach number 2.2 to 4.4Deployment and steady state performance of supersonic attached inflatable decelerator canopy models
Document ID
19700026642
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Bohon, H. L. (NASA Langley Research Center Hampton, VA, United States)
Miserentino, R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1970
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-5840
L-7023
Accession Number
70N35958
Funding Number(s)
CONTRACT_GRANT: 124-07-23-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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