NASA-LLIS-0127

Lessons Learned - Orbiter Protection System "Y" Curtain Wall Retraction

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T17:22:26Z
date available	2017-09-04T17:22:26Z
date copyright	08/25/1992
date issued	1992
identifier other	ZVYCQCAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std/handle/yse/145611
description abstract	Description of Driving Event: During the retraction of the orbiter protection system "Y" curtain wall in the console mode, the speed attained after leaving the slow travel transition is excessive. The operator must manipulate a manual valve to reduce air flow to the winch. High impact stops from the rapid movement of the "Y" curtain wall during retraction may cause personnel injury and/or damage to payloads and facility (PAD).
language	English
title	NASA-LLIS-0127	num
title	Lessons Learned - Orbiter Protection System "Y" Curtain Wall Retraction	en
type	standard
page	2
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1992
contenttype	fulltext
subject keywords	Facilities
subject keywords	Ground Equipment
subject keywords	Ground Operations