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NASA-LLIS-0361

Lessons Learned - Parachute Diameter and Pilot/Payload Descent Rate

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1995

Abstract: Description of Driving Event:
The X-31 experimental aircraft used the egress system from the F-18 fighter aircraft, including its 17 foot diameter main parachute. A test pilot ejected from the X-31 over Edwards Air Force Base, CA. The pilot's calculated descent rate was over 28 feet per second. The parachute landing fall resulted in multiple injuries.
URI: https://yse.yabesh.ir/std/handle/yse/9772
Subject: Aircraft
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
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    NASA-LLIS-0361

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:11:24Z
date available2017-09-04T15:11:24Z
date copyright34983
date issued1995
identifier otherLUAEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/9772
description abstractDescription of Driving Event:
The X-31 experimental aircraft used the egress system from the F-18 fighter aircraft, including its 17 foot diameter main parachute. A test pilot ejected from the X-31 over Edwards Air Force Base, CA. The pilot's calculated descent rate was over 28 feet per second. The parachute landing fall resulted in multiple injuries.
languageEnglish
titleNASA-LLIS-0361num
titleLessons Learned - Parachute Diameter and Pilot/Payload Descent Rateen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1995
contenttypefulltext
subject keywordsAircraft
subject keywordsEmergency Preparedness
subject keywordsFlight Equipment
subject keywordsPersonal Protective Equipment
subject keywordsSafety & Mission Assurance
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DSpace software copyright © 2017-2020  DuraSpace
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