NASA-LLIS-0705

Lessons Learned – Micrometeoroid Protection

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T17:00:58Z
date available	2017-09-04T17:00:58Z
date copyright	03/16/2000
date issued	2000
identifier other	XQCEQCAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/124467
description abstract	Abstract: Preferred Practice for Design & Test. The absence of micrometeoroid protection measures in spacecraft and mission design will increase the risk of significant damage to the spacecraft, particularly in areas of high meteoroid flux and during vulnerable mission phases. Provide protection for the spacecraft structure and instruments to minimize damage from micrometeoroid penetration. Typical reliability engineering measures range from structural positioning to protect sensitive hardware to placement of protective blankets on the spacecraft exterior.
language	English
title	NASA-LLIS-0705	num
title	Lessons Learned – Micrometeoroid Protection	en
type	standard
page	9
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;2000
contenttype	fulltext