1.1This test method covers the estimation of the net heat of combustion at constant pressure in SI units (megajoules per kilogram) or inch-pound units [Btu per pound].
1.2This test method is purely empirical and is applicable only to liquid hydrocarbon fuels derived by normal refining processes from conventional crude oil, which conform to the requirements of specifications for aviation gasolines, or aircraft turbine and jet engine fuels of limited boiling ranges and compositions as described in Note 1.
| Fuel | Specification |
| Aviation gasoline fuels: | Specification D910 |
| Grades 80, 82, 100/130, and 115/145 | Specification D6227 |
| DEF STAN 91-90 | |
| NATO Code F-18 | |
|
| |
| Aviation turbine fuels: | MIL-DTL-5624 |
| JP-4,Avtag/FSII | DEF STAN 91-88 |
| NATO Code F-40 | |
|
| |
| JP-5,Avcat/FSII | MIL-DTL-5624 |
| DEF STAN 91-86 | |
| NATO Code F-44 | |
|
| |
| Jet A, Jet A-1, Avtur | Specification D1655 |
| DEF STAN 91-91 | |
| NATO Code F-35 | |
1.3This test method is not applicable to pure hydrocarbons. It is not intended as a substitute for experimental measurements of heat of combustion.
1.4The heat of combustion may also be determined in SI units by Test Method D4529. Test Method D4529 requires calculation of a single equation for all aviation fuels with a precision equivalent to that of this test method.
1.5The values stated in either SI units or inch-pound units are to be regarded separately as standard. The values stated in each system may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the two systems may result in non-conformance with the standard.
1.6This 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.
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