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Parachute Testing at Altitudes Between 30 and 90 KilometersHigh altitude parachute systems test techniques for analysis of inflation, stability variations, porosity, effects at low dynamic pressure, etc
Document ID
19660061312
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Gapcynski, J. P.
Mcfall, John C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Murrow, Harold N. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: AIAA Aerodynamic Deceleration Systems Conference
Location: Houston, TX
Country: United States
Start Date: September 7, 1966
End Date: September 9, 1966
Sponsors: American Inst. of Aeronautics and Astronautics
Accession Number
66A40602
Distribution Limits
Public
Copyright
Other
Keywords
HIGH ALTITUDE TESTING
PRESSURE EFFECT
PARACHUTE

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