MIL-DTL-25524E
TURBINE FUEL, AVIATION, THERMALLY STABLE
contributor author | AIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City | |
date accessioned | 2017-09-04T15:06:13Z | |
date available | 2017-09-04T15:06:13Z | |
date copyright | 35754 | |
date issued | 1997 | |
identifier other | LEHBEAAAAAAAAAAA.pdf | |
identifier uri | http://yse.yabesh.ir/std;query=anid=/handle/yse/3755 | |
description abstract | This specification was thoroughly reviewed as a part of acquisition reform. While most of the requirements were converted to performance terms, due to the military-unique nature of the product (see 6.1) and the need for compatibility with deployed systems, it was determined that not all requirements could be converted. The issuance of this specification as "detail" is not intended to constrain technology advances in future systems. This specification covers one grade of turbine fuel designated as JPTS (see 6.1). Intended Use: The fuel covered by this specification is intended for use in aircraft turbine engines (see 1.1). | |
language | English | |
title | MIL-DTL-25524E | num |
title | TURBINE FUEL, AVIATION, THERMALLY STABLE | en |
type | standard | |
page | 11 | |
status | Active | |
tree | AIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City:;1997 | |
contenttype | fulltext | |
subject keywords | additive | |
subject keywords | antioxidant | |
subject keywords | corrosion inhibitor | |
subject keywords | deactivator | |
subject keywords | flash point | |
subject keywords | fuel system icing inhibitor | |
subject keywords | jet fuel | |
subject keywords | lubricity improver |