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Flight test of a 31.2-foot-diameter modified ringsail parachute deployed at a Mach number of 1.39 and a dynamic pressure of 11.0 pounds per square footFlight test of 31.2-foot-diameter modified ringsail parachute deployed at Mach 1.39 and dynamic pressure of 11 pounds per square foot
Document ID
19670022936
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Eckstrom, C. V. (NASA Langley Research Center Hampton, VA, United States)
Murrow, H. N. (NASA Langley Research Center Hampton, VA, United States)
Preisser, J. S. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-1414
Accession Number
67N32265
Funding Number(s)
CONTRACT_GRANT: 709-08-00-D1-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLIGHT TEST
AERODYNAMIC CHARACTERISTICS
PARACHUTE

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