NASA-LLIS-0128

Lessons Learned - Main Landing Gear (MLG) Tire Rupture During Postlanding Operations

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T17:31:17Z
date available	2017-09-04T17:31:17Z
date copyright	08/26/1992
date issued	1992
identifier other	CWYCQCAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std/handle/yse/154202
description abstract	Description of Driving Event: MLG tire heat generated from max. Braking due to a crosswind landing, heavy orbiter, or long landing, could cause a transfer of heat to continue to the MLG tires after wheel stop, resulting in a delayed tire blowout. An explosive tire rupture caused by increasing tire pressure, cuts, excessive loading, or skidding could injure personnel and/or damage the orbiter/chassis hydraulic system/ ground support equipment. Three thermal relief plugs in each MLG tire prevent tire overpressurization, the orbiter anti-skid/brake control system prevents locked brakes, and the orbiter hydraulic system displacement limiter limits hydraulic fluid loss.
language	English
title	NASA-LLIS-0128	num
title	Lessons Learned - Main Landing Gear (MLG) Tire Rupture During Postlanding Operations	en
type	standard
page	2
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1992
contenttype	fulltext
subject keywords	Fire Protection
subject keywords	Flight Equipment
subject keywords	Ground Operations