NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
AERODYNAMIC DRAG AND STABILITY CHARACTERISTICS OF TOWED INFLATABLE DECELERATORS AT SUPERSONIC SPEEDSAerodynamic drag and stability of towed inflatable decelerators at supersonic speeds
Document ID
19630003840
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Mc Shera, J. T., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-1601
Report Number: NASA-TN-D-1601
Accession Number
63N13716
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC SPEED
DRAG
AERODYNAMIC STABILITY
DECELERATOR
TOWED BODY
INFLATABLE DEVICE

Related Records

There are no records associated with this record.
No Preview Available