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NASA-TN-D-6866

Summary of design considerations for airplane spin-recovery parachute systems

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1972

Abstract: A compilation of design considerations applicable to spin-recovery parachute systems for military airplanes has been made so that the information will be readily available to persons responsible for the design of such systems. This information was obtained from a study of available documents and from discussions with persons in both government and industry experienced in parachute technology, full-scale and model spin testing, and related systems.
URI: http://yse.yabesh.ir/std/handle/yse/169261
Subject: AERODYNAMIC
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    NASA-TN-D-6866

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:46:05Z
date available2017-09-04T17:46:05Z
date copyright01/01/1972
date issued1972
identifier otherEKYKAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/169261
description abstractA compilation of design considerations applicable to spin-recovery parachute systems for military airplanes has been made so that the information will be readily available to persons responsible for the design of such systems. This information was obtained from a study of available documents and from discussions with persons in both government and industry experienced in parachute technology, full-scale and model spin testing, and related systems.
languageEnglish
titleNASA-TN-D-6866num
titleSummary of design considerations for airplane spin-recovery parachute systemsen
typestandard
page60
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1972
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRCRAFT
subject keywordsCHUTES
subject keywordsCONFIGURATIONS
subject keywordsDEVELOPMENT
subject keywordsDRAG
subject keywordsENGINEERING
subject keywordsEQUIPMENT
subject keywordsMILITARY
subject keywordsPRODUCT
subject keywordsSPECIFICATIONS
subject keywordsSYSTEMS
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