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Development of an extremely lightweight, high- altitude deceleratorParachute design for decelerating upper atmosphere rocket probes at high altitudes, using high drag coefficients in Stokes flow regime
Document ID
19700039294
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Niederer, P. G.
Date Acquired
August 5, 2013
Publication Date
November 1, 1969
Subject Category
Aircraft
Report/Patent Number
AIAA PAPER 68-949
Report Number: AIAA PAPER 68-949
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AERODYNAMIC DECELERATION SYSTEMS CONFERENCE, 2ND
Location: EL CENTRO, CA
Start Date: September 23, 1968
End Date: September 25, 1968
Sponsors: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
70A15410
Funding Number(s)
CONTRACT_GRANT: NAS5-10168
CONTRACT_GRANT: NAS1-7770
Distribution Limits
Public
Copyright
Other

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