NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Performance of a 26-meter-diameter ringsail parachute in a simulated Martian environmentInflation, drag, and stability characteristics of 26-meter diameter ringsail parachute in simulated Martian environment
Document ID
19670009951
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bendura, R. J. (NASA Langley Research Center Hampton, VA, United States)
Coltrane, L. C. (NASA Langley Research Center Hampton, VA, United States)
Whitlock, C. H. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1967
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-1356
Accession Number
67N19280
Funding Number(s)
CONTRACT_GRANT: 709-08-00-01-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PARACHUTE
PERFORMANCE CHARACTERISTICS
MARS ENVIRONMENT

Related Records

IDRelationTitle20070031003Supplemented ByPerformance of 26 Meter Diameter Ringsail Parachute in a Simulated Martian Environment
No Preview Available