ASTM-D3241 › Standard Test Method for Thermal Oxidation Stability of Aviation Turbine Fuels
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Scope
1.1 This test method covers the procedure for rating the tendencies of gas turbine fuels to deposit decomposition products within the fuel system.
1.2 The values stated in SI units are to be regarded as the standard. The inch-pound values given in parentheses are for information only. The differential pressure values in mm Hg are defined only in terms of this test method.
1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use. For specific hazard statements, see 6.1.1, 7.2, 7.2.1, 7.3, 11.1.1, and Annex A3.
Keywords
differential pressure; fuel decomposition; oxidative deposits; test filter deposits; thermal stability; turbine fuel; ICS Number Code 75.160.20 (Liquid fuels)
To find similar documents by ASTM Volume:
05.01 (Petroleum Products and Lubricants (I): D56 - D3710)
To find similar documents by classification:
75.160.20 (Liquid fuels Including gasoline, diesel, kerosene, etc.)
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Document Number
ASTM-D3241-23AE01
Revision Level
2023A(E1) EDITION
Status
Current
Modification Type
Revision
Publication Date
Jan. 10, 2024
Document Type
Test Method
Page Count
25 pages
Committee Number
D02.J0