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    NAVY MIL-DTL-5624 V-2013 TURBINE FUEL AVIATION GRADES JP-4 AND JP-5.pdf

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    NAVY MIL-DTL-5624 V-2013 TURBINE FUEL AVIATION GRADES JP-4 AND JP-5.pdf

    1、 AMSC N/A FSC 9130 Comments, suggestions, or questions on this document should be addressed to: Commander, Naval Air Warfare Center Aircraft Division, Code 4L8000B120-3, Highway 547, Lakehurst, NJ 08733-5100 or emailed to michael.sikoranavy.mil. Since contact information can change, you may want to

    2、verify the currency of this address information using the ASSIST Online database at https:/assist.dla.mil. DETAIL SPECIFICATION TURBINE FUEL, AVIATION, GRADES JP-4 AND JP-5 This specification is approved for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This s

    3、pecification covers two grades of aviation turbine fuel NATO F-40 (JP-4) and NATO F-44 (JP-5) (see 6.1). Synthesized hydrocarbons from new sources require specific guidance that is outside the scope of MIL-DTL-5624. This guidance is found in ASTM D7566. 1.2 Classification. Aviation turbine fuel will

    4、 be of the following grades, as specified (see 6.2). Grade NATO Code No. Description JP-4 (Inactive for New Design) F-40 Wide cut, gasoline type JP-5 F-44 High flash point, kerosene type 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this section are specified in sections 3 and 4 of th

    5、is specification. This section does not include documents cited in other sections of this specification or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified r

    6、equirements of documents cited in sections 3 and 4 of this specification, whether or not they are listed. METRIC MIL-DTL-5624V 11 July 2013 SUPERSEDING MIL-DTL-5624U 05 January 2004Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-5624V 2 2.2 G

    7、overnment documents. 2.2.1 Specifications and standards. The following specifications and standards form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. INTERNATIONAL STANDARIZATION AGR

    8、EEMENTS STANAG 1135 Interchangeability of Fuels, Lubricants, and Associated Products Used by the Armed Forces of the North Atlantic Treaty Nations STANAG 3747 Guide Specifications (Minimum Quality Standards) for Aviation Turbine Fuels (F-24, F-27, F-34, F-35, F-40, and F-44) DEPARTMENT OF DEFENSE SP

    9、ECIFICATIONS MIL-PRF-25017 Inhibitor, Corrosion/Lubricity Improver, Fuel Soluble (NATO S-1747) (Metric) MIL-DTL-85470 Inhibitor, Icing, Fuel System, High Flash, NATO Code Number S-1745 (Metric) DEPARTMENT OF DEFENSE STANDARDS MIL-STD-290 Packaging and Marking of Petroleum and Related Products QUALIF

    10、IED PRODUCTS LIST QPL-25017 Inhibitor, Corrosion/Lubricity Improver, Fuel Soluble (NATO S-1747) (Metric) (Copies of these documents are available online at https:/assist.dla.mil/quicksearch/ or from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094

    11、.) 2.3 Non-Government publications. The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. ASTM INTERNATIONAL ASTM D56 Standard Test Method for Flash Point by Tag

    12、Closed Cup Tester ASTM D86 Standard Test Method for Distillation of Petroleum Products at Atmospheric Pressure ASTM D93 Standard Test Methods for Flash Point by Pensky-Martens Closed Cup Tester Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-

    13、5624V 3 ASTM D129 Standard Test Methods for Sulfur in Petroleum Products (General High Pressure Decomposition Device Method) ASTM D130 Standard Test Method for Corrossiveness to Copper from Petroleum Products by Copper Strip Test ASTM D156 Standard Test Method for Saybolt Color of Petroleum Products

    14、 (Saybolt Chromometer Method) ASTM D323 Standard Test Method for Vapor Pressure of Petroleum Products (Reid Method) ASTM D381 Standard Test Method for Gum Content in Fuels by Jet Evaporation ASTM D445 Standard Test Method for Kinematic Viscosity of Transparent and Opaque Liquids (and Calculation of

    15、Dynamic Viscosity) ASTM D976 Standard Test Method for Calculated Cetane Index of Distillate Fuels ASTM D1094 Standard Test Method for Water Reaction of Aviation Fuels ASTM D1266 Standard Test Method for Sulfur in Petroleum Products (Lamp Method) ASTM D1298 Standard Practice for Density, Relative Den

    16、sity, or API Gravity of Crude Petroleum and Liquid Petroleum Products by Hydrometer Method ASTM D1319 Standard Test Method for Hydrocarbon Types in Liquid Petroleum Products by Fluorescent Indicator Adsorption ASTM D1322 Standard Test Method for Smoke Point of Kerosine and Aviation Turbine Fuel ASTM

    17、 D2276 Standard Test Method for Particulate Contaminant in Aviation Fuel by Line Sampling ASTM D2386 Standard Test Method for Freezing Point of Aviation Fuels ASTM D2622 Standard Test Method for Sulfur in Petroleum Products by Wavelength Dispersive X-Ray Fluorescence Spectrometry ASTM D2624 Standard

    18、 Test Methods for Electrical Conductivity of Aviation and Distillate Fuels ASTM D2887 Standard Test Method for Boiling Range Distribution of Petroleum Fractions by Gas Chromatography ASTM D3120 Standard Test Method for Trace Quantities of Sulfur in Light Liquid Petroleum Hydrocarbons by Oxidative Mi

    19、crocoulometry ASTM D3227 Standard Test Method for (Thiol Mercaptan) Sulfur in Gasoline, Kerosine, Aviation Turbine, and Distillate Fuels (Potentiometric Method) ASTM D3241 Standard Test Method for Thermal Oxidation Stability of Aviation Turbine Fuels ASTM D3242 Standard Test Method for Acidity in Av

    20、iation Turbine Fuel Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-5624V 4 ASTM D3338 Standard Test Method for Estimation of Net Heat of Combustion of Aviation Fuels ASTM D3343 Standard Test Method for Estimation of Hydrogen Content of Aviat

    21、ion Fuels ASTM D3701 Standard Test Method for Hydrogen Content of Aviation Turbine Fuels by Low Resolution Nuclear Magnetic Resonance Spectrometry ASTM D3828 Standard Test Methods for Flash Point by Small Scale Closed Cup Tester ASTM D3948 Standard Test Method for Determining Water Separation Charac

    22、teristics of Aviation Turbine Fuels by Portable Separometer ASTM D4052 Standard Test Method for Density, Relative Density, and API Gravity of Liquids by Digital Density Meter ASTM D4057 Standard Practice for Manual Sampling of Petroleum and Petroleum Products ASTM D4177 Standard Practice for Automat

    23、ic Sampling of Petroleum and Petroleum Products ASTM D4294 Standard Test Method for Sulfur in Petroleum and in Petroleum Products by Energy-Dispersive X-Ray Fluorescence Spectrometry ASTM D4306 Standard Practice for Aviation Fuel Sample Containers for Tests Affected by Trace Contamination ASTM D4529

    24、 Standard Test Method for Estimation of Net Heat of Combustion of Aviation Fuels ASTM D4737 Standard Test Method for Calculated Cetane Index by Four Variable Equation ASTM D4809 Standard Test Method for Heat of Combustion of Liquid Hydrocarbon Fuels by Bomb Calorimeter (Precision Method) ASTM D4952

    25、Standard Test Method for Qualitative Analysis for Active Sulfur Species in Fuels and Solvents (Doctor Test) ASTM D4953 Standard Test Method for Vapor Pressure of Gasoline and Gasoline-Oxygenate Blends (Dry Method) ASTM D5001 Standard Test Method for Measurement of Lubricity of Aviation Turbine Fuels

    26、 by the Ball-on-Cylinder Lubricity Evaluator (BOCLE) ASTM D5006 Standard Test Method for Measurement of Fuel System Icing Inhibitors (Ether Type) in Aviation Fuels ASTM D5191 Standard Test Method for Vapor Pressure of Petroleum Products (Mini Method) ASTM D5452 Standard Test Method for Particulate C

    27、ontamination in Aviation Fuels by Laboratory Filtration Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-5624V 5 ASTM D5453 Standard Test Method for Determination of Total Sulfur in Light Hydrocarbons, Spark Ignition Engine Fuel, Diesel Engine

    28、 Fuel, and Engine Oils by Ultraviolet Fluorescence ASTM D5972 Standard Test Method for Freezing Point of Aviation Fuels (Automatic Phase Transition Method) ASTM D6045 Standard Test Method for Color of Petroleum Products by the Automatic Tristimulus Method ASTM D6890 Standard Test Method for Determin

    29、ation of Ignition Delay and Derived Cetane Number (DCN) of Diesel Fuel Oils by Combustion in a Constant Volume Chamber ASTM D7153 Standard Test Method for Freezing Point of Aviation Fuels (Automatic Laser Method) ASTM D7154 Standard Test Method for Freezing Point of Aviation Fuels (Automatic Fiber O

    30、ptical Method) ASTM D7170 Standard Test Method for Determination of Derived Cetane Number (DCN) of Diesel Fuel Oils-Fixed Range Injection Period, Constant Volume Combustion Chamber Method ASTM D7171 Standard Test Method for Hydrogen Content of Middle Distillate Petroleum Products by Low-Resolution P

    31、ulsed Nuclear Magnetic Resonance Spectroscopy ASTM D7224 Standard Test Method for Determining Water Separation Characteristics of Kerosene - Type Aviation Turbine Fuels Containing Additives by Portable Separometer ASTM D7566 Standard Specification for Aviation Turbine Fuel Containing Synthesized Hyd

    32、rocarbons ASTM D7777 Standard Test Method for Density, Relative Density, or API Gravity of Liquid Petroleum by Portable Digital Density Meter ASTM E29 Standard Practice for Using Significant Digits in Test Data to Determine Conformance with Specifications (Copies of these documents are available onl

    33、ine at www.astm.org or from ASTM International,100 Barr Harbor Drive, West Conshohocken, PA 19428-2959.) ENERGY INSTITUTE IP 540 Determination of the Existant Gum Content of Aviation Turbine Fuel - Jet Evaporation Method IP 564 Determination of the Level of Cleanliness of Aviation Turbine Fuel - Lab

    34、oratory Automatic Particle Counter Method IP 565 Determination of the Level of Cleanliness of Aviation Turbine Fuel - Portable Automatic Particle Counter Method IP 577 Determination of the Level of Cleanliness of Aviation Turbine Fuel - Automatic Particle Counter Method Using Light Extinction (Copie

    35、s of these documents are available online at http:/www.energyinst.org/ or from the Energy Institute, 61 New Cavendish Street, London, WIG 7AR, UK.) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-5624V 6 2.4 Order of precedence. Unless otherw

    36、ise noted herein or in the contract, in the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.

    37、3. REQUIREMENTS 3.1 Materials. The fuels supplied under this specification shall be refined hydrocarbon distillate fuel oils, which contain additives in accordance with 3.3. The feedstock from which the fuel is refined shall be crude oils derived from petroleum, oil sands, oil shale, synthesized hyd

    38、rocarbons, or mixtures thereof. 3.1.1 Synthesized Hydrocarbons (applies to Grade JP-5 fuel only). A maximum of 50 volume percent of the finished fuel may consist of Synthesized Paraffinic Kerosene (SPK) blend components derived from Hydroprocessed Esters and Fatty Acid (HEFA) or Fischer Tropsch (FT)

    39、 produced SPK. FT-SPK blend components shall conform to the requirements in ASTM D7566 Annex A1 with the exceptions as noted in Table I of this specification. SPK blend components derived from HEFA shall conform to requirements in ASTM D7566 Annex A2 with the exceptions as noted in Table I of this s

    40、pecification. Finished fuel containing synthesized hydrocarbons shall conform to the properties listed in Tables II and IV. Finished fuel containing synthesized hydrocarbons shall contain additives in accordance with 3.3 through 3.3.6. The U.S. Army is currently in the process of qualifying their re

    41、spective aircraft, ground vehicles, and equipment to use fuel containing SPK. Fuels containing synthetic blending components shall not be used in Army aircraft, ground vehicles, and equipment without approval from the following cognizant activities. Cognizant activities for the U.S. Army: U.S. Army

    42、Ground: Fuels and Lubricants Technology Team, RDECOM-TARDEC, RDTA-SIE-ES-FPT-FLT, Building 210, 6501 E. 11 Mile Road, Warren, MI 48397-5000. U.S. Army Aviation: U.S. Army RDECOM, Attn: RDMR-AEP, Building 4488, Room C-211, Redstone Arsenal, AL 35898-5000. Provided by IHSNot for ResaleNo reproduction

    43、or networking permitted without license from IHS-,-,-MIL-DTL-5624V 7 TABLE I. Requirements for Synthesized Paraffinic Kerosene blend components for JP-5 Fuel exceptions to ASTM D7566, annexes A1 and A2, Tables A1.1, A1.2, A2.1, and A2.2 detailed requirements. Note: Values in this table take preceden

    44、ce over any conflicting values in ASTM D7566. 1/ Referee Test Method. 2/ ASTM D3828 may give results up to 1.7 C below the ASTM D93 results. ASTM D56 may give results up to 1 C below the ASTM D93 results. 3.2 Finished fuel. Finished fuels shall meet the requirements of this specification. The requir

    45、ements of Table IV apply if the finished fuel contains synthesized hydrocarbons. 3.3 Additives. If specified in the contract or purchase order (see 6.2), information concerning the type and amount of each additive used shall be reported. 3.3.1 Antioxidants. Immediately after processing (i.e., during

    46、 the rundown into feed/batch tank) and before the fuel is exposed to the atmosphere, an approved antioxidant shall be added to all JP-5 fuel; and to JP-4 fuel that contains blending stocks that have been hydrogen treated to prevent the formation of gums and peroxides after manufacture. JP-4 fuel tha

    47、t does not contain hydrogen-treated blending stocks may have the antioxidant added. The concentration of antioxidant to be added shall be as follows: a. For JP-5 and hydrogen-treated JP-4: Not less than 17.2 mg nor more than 24.0 mg of active ingredient per liter of fuel (6.0 to 8.4 lb/1000 barrels)

    48、. b. For JP-4 fuel not hydrogen treated, if added, not more than 24.0 mg of active ingredient per liter of fuel (8.4 lb/1000 barrels). Property FT-SPK or HEFA-SPK ASTM Test Method Flash Point, C, min 60.0 D56, D931/2/, or D3828 Density at 15 C kg/L, min (API max) kg/L, max (API min) 0.750 (57.2) 0.7

    49、70 (52.3) D1298 or D40521/Freezing Point, C, max -46 D23861/, D5972, D7153, or D7154 Derived Cetane Number, min 40 D68901/or D7170 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-5624V 8 3.3.1.1 Formulations. The following antioxidant formulations are approved: a. 2,6-di-tert-butyl-4-methylphenol b. 6-tert-butyl-2,4-di


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