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AIA/NAS NAS3620
PROPELLANTS, NITROGEN TETROXIDE - Rev 2
| contributor author | AIA/NAS - Aerospace Industries Association of America Inc. | |
| date accessioned | 2017-09-04T16:04:29Z | |
| date available | 2017-09-04T16:04:29Z | |
| date copyright | 2013.05.31 | |
| date issued | 2013 | |
| identifier other | RTDNDFAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;quein/handle/yse/67711 | |
| description abstract | Purpose. This specification covers the requirements for three types of nitrogen tetroxide (N2O4) propellants with separate requirements for procurement and useIntended Use: The propellant described by this specification is intended for use as an oxidizer in rocket engines. | |
| language | English | |
| title | AIA/NAS NAS3620 | num |
| title | PROPELLANTS, NITROGEN TETROXIDE - Rev 2 | en |
| type | standard | |
| page | 32 | |
| status | Not for New Design | |
| tree | AIA/NAS - Aerospace Industries Association of America Inc.:;2013 | |
| contenttype | fulltext |
