NASA-LLIS-3116

Lessons Learned - Bent Orbital Maneuvering System (OMS) Pod Rotato

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:43:38Z
date available	2017-09-04T18:43:38Z
date copyright	04/21/2010
date issued	2010
identifier other	KCMGFDAAAAAAAAAA.pdf
identifier uri	https://lib.yabesh.ir/std/handle/yse/225028
description abstract	Abstract: The Space Shuttle Orbital Maneuvering System (OMS) pod rotator (a 5-ton jack screw) was bent on three occasions because of overloading. As a result, Boeing designed a system consisting of two load-sensing pins: one pin for attaching the rotator to the OMS pod lifting fixture and the other for attaching the rotator to the facility attachment point. Each sensing pin is connected to a readout unit to indicate when the rotator is under load or when the rotator load changes between tension and compression. Two load-sensing pins are used for redundancy.
language	English
title	NASA-LLIS-3116	num
title	Lessons Learned - Bent Orbital Maneuvering System (OMS) Pod Rotato	en
type	standard
page	1
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;2010
contenttype	fulltext
subject keywords	Ground Equipment
subject keywords	Hardware
subject keywords	Lifting Devices
subject keywords	Simulators and Training Systems
subject keywords	Systems analysis - cost analysis
subject keywords	Vehicle concepts