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Lessons Learned – Rigor in Integrated Design, Development, Documentation, and Configuration Control

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:43:25Z
date available2017-09-04T16:43:25Z
date copyright02/29/2000
date issued2000
identifier otherVUCEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/106657
description abstractDescription of Driving Event:
On December 8, 1995, a full-scale model of the NASA JSC Experimental Crew Return Vehicle (XCRV) experienced a failure of its parafoil deployment system during a test drop at the U.S. Army's Yuma Proving Ground (YPG) near Yuma, Arizona. The wingless 24-foot model impacted the ground without the parafoil deployed due to damage sustained when two lines entangled during deployment from a Colorado Air National Guard C-130 Aircraft at 15,000 feet mean sea level. The design of the test-unique model, platform restraint and separation system was neither reviewed by all parties affected by its integration nor well documented. As a result, opportunities to identify design problems were missed, and there was little opportunity to ensure conformance with the intended design in the vehicle configuration process.
languageEnglish
titleNASA-LLIS-0743num
titleLessons Learned – Rigor in Integrated Design, Development, Documentation, and Configuration Controlen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2000
contenttypefulltext
subject keywordsAircraft
subject keywordsConfiguration Management
subject keywordsFlight Equipment
subject keywordsFlight Operations
subject keywordsHardware
subject keywordsPolicy & Planning
subject keywordsResearch & Development
subject keywordsRisk Management/Assessment
subject keywordsTest & Verification
subject keywordsTest Article


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