AIAA S-113
Criteria for Explosive Systems and Devices on Space and Launch Vehicles
Year: 2005
Abstract: This standard establishes criteria for design, manufacture, and performance certification of explosive systems and explosive devices commonly used on launch, upper stage, and space vehicle systems. The requirements contained in this specification are intended to serve as a universal set of tools for use by explosive system manufacturers and users during all phases of development and certification to assure safe application and high quality products. This information may also be used for guidance during preparation of acquisition contracts and program-specific documents, and may be used for explosive system applications unrelated to space vehicles.
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contributor author | AIAA - American Institute of Aeronautics and Astronautics | |
date accessioned | 2017-09-04T15:17:27Z | |
date available | 2017-09-04T15:17:27Z | |
date copyright | 2005.11.10 | |
date issued | 2005 | |
identifier other | MNBRIBAAAAAAAAAA.pdf | |
identifier uri | http://yse.yabesh.ir/std;jsery=autho4703177D081D20686159DD6EFDEC9FCD/handle/yse/16897 | |
description abstract | This standard establishes criteria for design, manufacture, and performance certification of explosive systems and explosive devices commonly used on launch, upper stage, and space vehicle systems. The requirements contained in this specification are intended to serve as a universal set of tools for use by explosive system manufacturers and users during all phases of development and certification to assure safe application and high quality products. This information may also be used for guidance during preparation of acquisition contracts and program-specific documents, and may be used for explosive system applications unrelated to space vehicles. | |
language | English | |
title | AIAA S-113 | num |
title | Criteria for Explosive Systems and Devices on Space and Launch Vehicles | en |
type | standard | |
page | 121 | |
status | Active | |
tree | AIAA - American Institute of Aeronautics and Astronautics:;2005 | |
contenttype | fulltext |