MIL-PRF-26536F
PROPELLANT, HYDRAZINE
Year: 2011
Abstract: This specification covers the requirements for three grades of hydrazine (N2H4).Intended Use: The propellant described by this specification is intended for use as a fuel in rocket engines.
Subject: Catalytic Engine
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contributor author | AIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering) | |
date accessioned | 2017-09-04T18:47:33Z | |
date available | 2017-09-04T18:47:33Z | |
date copyright | 04/01/2011 | |
date issued | 2011 | |
identifier other | KMFNGEAAAAAAAAAA.pdf | |
identifier uri | http://yse.yabesh.ir/std/handle/yse/228709 | |
description abstract | This specification covers the requirements for three grades of hydrazine (N2H4).Intended Use: The propellant described by this specification is intended for use as a fuel in rocket engines. | |
language | English | |
title | MIL-PRF-26536F | num |
title | PROPELLANT, HYDRAZINE | en |
type | standard | |
page | 36 | |
status | Active | |
tree | AIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering):;2011 | |
contenttype | fulltext | |
subject keywords | Catalytic Engine | |
subject keywords | Fuel | |
subject keywords | Monopropellant | |
subject keywords | Rocket Engine |