SMC-S-005

SPACE SYSTEMS – FLIGHT PRESSURIZED SYSTEMS

contributor author	AIR FORCE - 02 - Air Force Network Integration Center (AFNIC)
date accessioned	2017-09-04T18:47:50Z
date available	2017-09-04T18:47:50Z
date copyright	06/03/2009
date issued	2009
identifier other	KNDQJEAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/229072
description abstract	This document establishes the baseline requirements for the design, fabrication, assembly, installation, test, inspection, operation, and maintenance of pressure systems used in spacecraft and launch vehicles. It deals primarily with the interfaces between the pressure vessel(s), or pressurized structures, and the corresponding pressure components within a specific pressure system; and interfaces between a pressure system and other spacecraft or launch vehicle systems. These requirements, when implemented on a specific pressure system, will assure a high level of confidence in achieving safe and reliable operation.
language	English
title	SMC-S-005	num
title	SPACE SYSTEMS – FLIGHT PRESSURIZED SYSTEMS	en
type	standard
page	35
status	Active
tree	AIR FORCE - 02 - Air Force Network Integration Center (AFNIC):;2009
contenttype	fulltext