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PROPELLANT, HIGH DENSITY SYNTHETIC HYDROCARBON TYPE, GRADE JP-10

contributor authorAIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering)
date accessioned2017-09-04T17:40:15Z
date available2017-09-04T17:40:15Z
date copyright01/12/2012
date issued2012
identifier otherDUXUTEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/163297
description abstractThis 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.
languageEnglish
titleMIL-DTL-87107Enum
titlePROPELLANT, HIGH DENSITY SYNTHETIC HYDROCARBON TYPE, GRADE JP-10en
typestandard
page12
statusActive
treeAIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering):;2012
contenttypefulltext
subject keywordsexo-Tetrahydrodicyclopentadiene
subject keywordsMissile Fuel
subject keywordsRamjet


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