MIL-DTL-87107E
PROPELLANT, HIGH DENSITY SYNTHETIC HYDROCARBON TYPE, GRADE JP-10
contributor author | AIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering) | |
date accessioned | 2017-09-04T17:40:15Z | |
date available | 2017-09-04T17:40:15Z | |
date copyright | 01/12/2012 | |
date issued | 2012 | |
identifier other | DUXUTEAAAAAAAAAA.pdf | |
identifier uri | https://yse.yabesh.ir/std/handle/yse/163297 | |
description abstract | This specification covers one grade of high density synthetic hydrocarbon type propellant.Intended Use: The fuel covered by this specification is intended for use in military gas turbine engines or military ramjet engines for missile application. | |
language | English | |
title | MIL-DTL-87107E | num |
title | PROPELLANT, HIGH DENSITY SYNTHETIC HYDROCARBON TYPE, GRADE JP-10 | en |
type | standard | |
page | 12 | |
status | Active | |
tree | AIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering):;2012 | |
contenttype | fulltext | |
subject keywords | exo-Tetrahydrodicyclopentadiene | |
subject keywords | Missile Fuel | |
subject keywords | Ramjet |