درباره ما
MIL-DTL-87107E
PROPELLANT, HIGH DENSITY SYNTHETIC HYDROCARBON TYPE, GRADE JP-10
Year: 2012
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.
Subject: exo-Tetrahydrodicyclopentadiene
Show full item record
| 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 |