ASTM D 4529 : 2017 : REDLINE
Current
The latest, up-to-date edition.
English
01-01-2017
CONTAINED IN VOL. 05.02, 2017 Explains the estimation of the net heat of combustion at constant pressure in metric (SI) units, megajoules per kilogram.
1.1This test method covers the estimation of the net heat of combustion at constant pressure in metric (SI) units, megajoules per kilogram.
1.2This test method is purely empirical, and it 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.
Note 1:The estimation of the net heat of combustion of a hydrocarbon fuel from its aniline point temperature and density is justifiable only when the fuel belongs to a well-defined class for which a relationship between these quantities has been derived from accurate experimental measurements on representative samples of that class. Even in this class, the possibility that the estimates can be in error by large amounts for individual fuels should be recognized. The JP-8 fuel, although not experimentally tested, has properties similar to JP-5 and Jet A fuels and can be considered in the same class. The classes of fuels used to establish the correlation presented in this test method are represented by the following applications: Fuel Specification Aviation gasoline fuels: Specification D910 Grades 80, UL82, UL87, 90, 91, UL91, 94, UL94, 100/100LL/100VLL Specification D6227 Aviation turbine fuels: Specification D6615 Jet B, JP-4 MIL-DTL-5624 JP-5 MIL-DTL-5624 JP-8 MIL-DTL-83133 Jet A, Jet A-1 Specification D1655
Specification D7547
Specification D7592
Specification D7223
Specification D7566
1.3The net heat of combustion can also be estimated by Test Methods D1405 or D3338. Test Method D1405 requires calculation of one of four equations dependent on the fuel type with the precision equivalent to that of this test method, whereas Test Method D3338 requires calculation of a single equation for aviation fuel with a precision equivalent to that test method.
1.4The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.
1.5This 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.
| Committee |
D 02
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| DevelopmentNote |
Also numbered as IP 381 (04/2001)
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| DocumentType |
Redline
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| Pages |
5
|
| PublisherName |
American Society for Testing and Materials
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| Status |
Current
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| DEFSTAN 91-91/4(2002) : 2002 AMD 1 2004 | TURBINE FUEL, AVIATION KEROSENE TYPE, JET A-1 NATO CODE: F-35 JOINT SERVICE DESIGNATION: AVTUR |
| MIL-DTL-83133 Revision J:2015 | TURBINE FUEL, AVIATION, KEROSENE TYPE, JP-8 (NATO F-34), NATO F-35, AND JP-8+100 (NATO F-37) |
| DEFSTAN 91-88/1(1997) : 1997 | TURBINE FUEL, AVIATION: WIDE CUT TYPE, CONTAINING FUEL SYSTEM ICING INHIBITOR - NATO CODE: F-40 - JOINT SERVICE DESIGNATION: AVTAG/FSII |
| SAE J 1498 : 2017 | HEATING VALUE OF FUELS |
| ASTM D 3338/D3338M : 2009 : R2014 : EDT 1 | Standard Test Method for Estimation of Net Heat of Combustion of Aviation Fuels |
| MIL-DTL-83133 Revision K:2018 | TURBINE FUEL, AVIATION, KEROSENE TYPE, JP-8 (NATO F-34), NATO F-35, AND JP-8+100 (NATO F-37) |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-DTL-25524 Revision F:2015 | TURBINE FUEL, AVIATION, THERMALLY STABLE (JPTS) |
| DEFSTAN 91-87/4(2002) : 2002 | TURBINE FUEL, AVIATION KEROSENE TYPE, CONTAINING FUEL SYSTEM ICING INHIBITOR NATO CODE: F-34 JOINT SERVICE DESIGNATION: AVTUR/FSII |
| DEFSTAN 91-90/4(2015) : 2015 | GASOLINE AVIATION: GRADES UL91, 100/130 AND 100/130LL JOINT SERVICE DESIGNATION: AVGAS 100 AND AVGAS 100LL |
| IES RP 27.3:2017 | Recommended Practice for Photobiological Safety for Lamps – Risk Group Classification and Labeling |
| MIL-HDBK-510 Revision A:2014 | AEROSPACE FUELS CERTIFICATION |
| MIL PRF 5624 : S | TURBINE FUEL, AVIATION, GRADES JP-4, JP-5 AND JP-5/JP-8 ST |
| DEFSTAN 91-87/3(2002) : 2002 | TURBINE FUEL, AVIATION KEROSENE TYPE, CONTAINING FUEL SYSTEM ICING INHIBITOR NATO CODE: F-34 JOINT SERVICE DESIGNATION: AVTUR/FSII |
| DEFSTAN 91-90/3(2009) : 2009 | GASOLINE AVIATION: GRADES 80/87, 100/130 AND 100/130LL - JOINT SERVICE DESIGNATION: AVGAS 80, AVGAS 100 AND AVGAS 100LL |
| ASTM D 1655 : 2018-01 | SPECIFICATION FOR AVIATION TURBINE FUELS |
| ASTM D 1405/D1405M : 2008 | Standard Test Method for Estimation of Net Heat of Combustion of Aviation Fuels |
| DEFSTAN 91-86/4(2002) : 2002 | TURBINE FUEL, AVIATION KEROSENE TYPE: HIGH FLASH TYPE, CONTAINING FUEL SYSTEM ICING INHIBITOR NATO CODE: F-44 JOINT SERVICE DESIGNATION: AVCAT/FSII |
| MIL-HDBK-510-1 Revision A:2010 | AEROSPACE FUELS CERTIFICATION |
| DEFSTAN 91-86/2(1997) : 1997 | TURBINE FUEL, AVIATION: HIGH FLASH TYPE, CONTAINING FUEL SYSTEM ICING INHIBITOR - NATO CODE: F-44 - JOINT SERVICE DESIGNATION: AVCAT/FSII |
| MIL-DTL-5624 Revision W:2016 | TURBINE FUEL, AVIATION, GRADES JP-4 AND JP-5 |
| DEFSTAN 91-91/2(1996) : 1996 AMD 3 1998 | TURBINE FUEL, AVIATION KEROSENE TYPE, JET A-1 - NATO CODE: F-35 JOINT SERVICE DESIGNATION: AVTUR |
| DEFSTAN 91-88/2(2002) : 2002 | TURBINE FUEL, AVIATION: WIDE CUT TYPE, CONTAINING FUEL SYSTEM ICING INHIBITOR NATO CODE: F-40 JOINT SERVICE DESIGNATION: AVTAG/FSII |
| DEFSTAN 91-90/1(1996) : 1996 | GASOLINE, AVIATION: GRADES 80/87, 100/130 AND 100/130 LOW LEAD - JOINT SERVICE DESIGNATION: AVGAS 80, AVGAS 100 AND AVGAS 100LL |
| ASTM D 910 : 2017-05 | SPECIFICATION FOR LEADED AVIATION GASOLINES |
| ASTM D 7223 : 2017 : REDLINE | Standard Specification for Aviation Certification Turbine Fuel |
| ASTM D 4868 : 2017 : REDLINE | Standard Test Method for Estimation of Net and Gross Heat of Combustion of Hydrocarbon Burner and Diesel Fuels |
| DEFSTAN 91-87/1(1994) : INTERIM | TURBINE FUEL, AVIATION, KEROSINE TYPE CONTAINING FUEL SYSTEM ICING INHIBITOR NATO CODE: F-34 JOINT SERVICE DESIGNATION: AVTUR/FSII |
| ASTM D 3338/D3338M : 2009 : R2014 : EDT 2 | Standard Test Method for Estimation of Net Heat of Combustion of Aviation Fuels |
| DEFSTAN 91-86/3(2002) : 2002 | TURBINE FUEL, AVIATION KEROSENE TYPE: HIGH FLASH TYPE, CONTAINING FUEL SYSTEM ICING INHIBITOR NATO CODE: F-44 JOINT SERVICE DESIGNATION: AVCAT/FSII |
| DEFSTAN 91-86/1(1994) : INTERIM | TURBINE FUEL, AVIATION, HIGH FLASH TYPE CONTAINING FUEL SYSTEM ICING INHIBITOR NATO CODE: F-44 JOINT SERVICE DESIGNATION: AVCAT/FSII |
| DEFSTAN 91-90/2(2006) : 2006 | GASOLINE, AVIATION: GRADES 80/87, 100/130 AND 100/130 LOW LEAD - JOINT SERVICE DESIGNATION: AVGAS 80, AVGAS 100 AND AVGAS 100LL |
| ASTM D 1405/D1405M : 2008 : R2013 | Standard Test Method for Estimation of Net Heat of Combustion of Aviation Fuels (Withdrawn 2019) |
| ASTM D 8147 : 2017 | Standard Specification for Special-Purpose Test Fuels for Aviation Compression-Ignition Engines |
| ASTM D 3338/D3338M : 2009 | Standard Test Method for Estimation of Net Heat of Combustion of Aviation Fuels |
| ASTM D 3338/D3338M : 2009 : R2014 | Standard Test Method for Estimation of Net Heat of Combustion of Aviation Fuels |
| ASTM D 7960 : 2018 : REDLINE | Standard Specification for Unleaded Aviation Gasoline Test Fuel Containing Non-hydrocarbon Components |
| MIL-DTL-5624 Revision W:2016 | TURBINE FUEL, AVIATION, GRADES JP-4 AND JP-5 |
| ASTM D 941 : 1988 | Test Method for Density and Relative Density (Specific Gravity) of Liquids by Lipkin Bicapillary Pycnometer (Withdrawn 1993) |
| ASTM D 1217 : 2015 : REDLINE | Standard Test Method for Density and Relative Density (Specific Gravity) of Liquids by Bingham Pycnometer |
| ASTM D 129 : 2013-08 | TEST METHOD FOR SULFUR IN PETROLEUM PRODUCTS (GENERAL HIGH PRESSURE DECOMPOSITION DEVICE METHOD) |
| ASTM D 7223 : 2017 : REDLINE | Standard Specification for Aviation Certification Turbine Fuel |
| ASTM D 910 : 2017-05 | SPECIFICATION FOR LEADED AVIATION GASOLINES |
| MIL-DTL-83133 Revision J:2015 | TURBINE FUEL, AVIATION, KEROSENE TYPE, JP-8 (NATO F-34), NATO F-35, AND JP-8+100 (NATO F-37) |
| ASTM D 240 : 2017 : REDLINE | Standard Test Method for Heat of Combustion of Liquid Hydrocarbon Fuels by Bomb Calorimeter |
| ASTM D 2622 : 2016 : REDLINE | Standard Test Method for Sulfur in Petroleum Products by Wavelength Dispersive X-ray Fluorescence Spectrometry |
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