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Preliminary analytical investigation of booster recovery by use of a hot-air balloon for both deceleration and final recoveryFlight mechanics, aerodynamic heating, and system weight determinations for hot-air balloon booster recovery system
Document ID
19660027976
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Dunavant, J. C.
(NASA Langley Research Center Hampton, VA, United States)
Scher, S. H.
(NASA Langley Research Center Hampton, VA, United States)
Young, I. G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1966
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-3661
Report Number: NASA-TN-D-3661
Accession Number
66N37266
Funding Number(s)
CONTRACT_GRANT: 124-07-03-06-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BALLOON
WEIGHT ANALYSIS
BOOSTER RECOVERY
AERODYNAMIC HEATING
FLIGHT MECHANICS
RECOVERY DEVICE
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