NASA-LLIS-0123

Lessons Learned - Loads Imposed on Stabilizing Frame During Mate/demate Operations

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:20:16Z
date available	2017-09-04T18:20:16Z
date copyright	08/19/1992
date issued	1992
identifier other	HVYCQCAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/202864
description abstract	Description of Driving Event: The H70-0743 sling assembly consists of a forward and aft spreader beam assembly connected together by a segmented stabilizing frame assembly. With the two mobile crane concept, the sling assembly is used to lift and demate the orbiter to the shuttle carrier aircraft. At the contingency landing site, the two mobile crane concept is used with a 800-ton T-C 4000 truck crane for the aft lift and a 250-ton link belt for the forward lift. Visual observation must be maintained at all times during hoisting operations due to extremely limited clearances between the orbiter and facilities.
language	English
title	NASA-LLIS-0123	num
title	Lessons Learned - Loads Imposed on Stabilizing Frame During Mate/demate Operations	en
type	standard
page	2
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1992
contenttype	fulltext
subject keywords	Ground Operations
subject keywords	Industrial Operations
subject keywords	Lifting Devices
subject keywords	Transportation