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Gas Turbines Jet Engines Aircraft Mil-Specs - FSC 2840

AFGS-87271 - Engines, Unmanned Air Vehicle, Airbreathing Gas Turbine, Expendable

This specification establishes the performance, functional operation, durability, reliability, maintainability of subsystems, physical characteristics, and installation interface requirements for expendable airbreathing gas turbine engines used in unmanned air vehicles (UAVs). It establishes the inspections, analyses, demonstrations, and tests necessary to verify compliance with the stated requirements.

MIL-D-17984 - Data Presentation Requirements, Installed Performance And Air Induction Systems (Asg)

This specification covers requirements for presentation of performance characteristics of power plant installations and inlet geometry systems, as follows, for all ramjet, pulse jet, turbojet, turboprop, and other air-breathing-type propulation systems other than reciprocating engines for all piloted aircraft, guided missiles, and target drones.

MIL-E-008593 - Engines, Aircraft, Turboshaft And Turboprop, General Specification For

MIL-E-25149 - Engines, Aircraft, Turbo-Prop, Production Quality (S/S By X-28653)

MIL-E-38368 - Engine, Aircraft, Experimental Lift Turbojet, Preliminary Qualification Tests For (S/S By Mil-E-5007)

MIL-E-5007 - ( Images) Engine, Aircraft, Turbojet And Turbofan, General Specification For

This specification establishes the performance, operating characteristics, design features, detailed interface configuration definitions, and installation envelopes of turbojet and turbofan engines.

MIL-E-5008 - Engine, Aircraft, Turbojet, Model Specifications For, Outline And Instructions For Preparation (Use Mil-E-5007)

MIL-E-5009 - Engine, Aircraft, Turbojet And Turbofan, Tests For (Use Mil-E-5007)

MIL-E-5010 - Engine, Aircraft, Turbojet, Acceptance Test For

MIL-E-5156 - Engine, Aircraft, Experiment Turbojet Preliminary Flight Rating Tests For

MIL-E-5445 - Engines, Aircraft, Ground Test For Combat Power (War Emergency Rating)

MIL-E-5595 - Engine, Aircraft, Gas Turbine, Corrosion-Prevention Pre-Oiling And Ground Operation Of, Processes For

This specification covers the detail requirements governing the corrosion-prevention pre-oiling and ground operation of aircraft gas turbine engines and is applicable to all contractors having physical custody of these engines.

MIL-E-7389 - Engines, Aircraft, Turbojet Production Quality Control, Test For

MIL-E-8593 - ( Images) Engines, Aircraft, Turboshaft And Turboprop, General Specification For

MIL-E-8594 - Engine, Aircraft, Turboprop, Model Specification For (Outline And Instructions For Preparation) (Asg) (S/S By Mil-E-8593)

MIL-E-8595 - Engine, Aircraft, Turboprop, Qualification Test For (Asg) (S/S By Mil-E-8593)

MIL-E-8596 - Engine, Aircraft, Turboprop, Acceptance Tests For (Asg) (S/S By Mil-E-8593)

MIL-E-8597 - Engine, Aircraft, Experimental Turboprop Preliminary Flight Rating Tesss For (Asg) (S/S By Mil-E-8593)

MIL-E-87231 - Engines, Aircraft, Turbojet And Turbofan (S/S By Jsgs-87231)

This specification establishes the performance, functional operation, durability, reliability, maintainability of subsystems, physical characteristics, and installation interface requirements for aircraft turbojet and turbofan engines. It establishes the inspections, analyses, demonstrations and tests necessary to verify compliance with the stated requirements.

MIL-E-87236 - Engine, Air Vehicle, Ramjet

This specification establishes the performance, functional operation, structures life, propulsion system installation interface requirements and characteristics; and establishes the demonstration, tests, inspections, and analysis for the required development and acceptance of the ramjet, air vehicle engine.

MIL-E-9362 - Engine, Aircraft, Pulsejet, General Specification For

MIL-E-9363 - Engine, Aircraft, Pulsejet, Model Specification For Outline And Instructions For Preparation Of

MIL-E-9364 - Engine, Aircraft, Pulsejet Qualification Test For

MIL-E-9365 - Engines, Aircraft, Pulsejet Acceptance Test For

MIL-E-9366 - Engine, Aircraft, Pulsejet, Preliminary Flight Rating Tests For

MIL-I-5598 - Indicator, Turbine Time

MIL-I-83294 - Installation Requirement, Aircraft Propulsion Systems, General Specification For

MIL-I-87239 - Installation, Engine

MIL-P-85486 - Power Unit Auxiliary, S-3A Aircraft Equipment Specification For

This specification establishes the performance, operating characteristics, design features, detailed interface configuration definitions, and installation envelopes for a gas turbine auxiliary power unit (APU) with a government furnished equipment (GFE) electrical generator attached. The APU will be operated aboard the S-3A aircraft.

MIL-S-25057 - Screen System, Air Inlet, Aircraft Turbine Engine, General Specification For

MIL-S-4821 - Screens, Ground Protective, Jet Aircraft Intake Duct, (S/S By Mil-S-87233)

MIL-STD-1529 - Vendor Substantiation For Aerospace Propulsion System Items

Initital qualification tests serve the dual purpose of establishing qualification approval of both the design of an aerospace propulsion system and the fabrication sources of propulsion system items. However, such approval applies only to those fabrication sources whose items were represented in the specific aerospace propulsion system which satisfactorily passed the qualification tests. Substantiation tests have the single objective of proving the ability of an alternate source to process, fabricate, and manufacture aerospace propulsion system items which are at least equal in quality to those items on the latest or current production aerospace propulsion system.

MIL-STD-1534 - Engine, Aircraft, Gas Turbine, Technical Design Requirements

MIL-STD-1559 - Numbers, Serial, Aircraft Gas Turbine Engine And Engine Module Assignment Of (S/S By Mil-Hdbk-1559)

MIL-STD-1675 - Mass Properties & Design Data Reporting Forms Of Turbine Engines - Av (S/S By Mil-E-5007)

MIL-STD-1783 - Engine Structural Integrity Program (Ensip) (S/S By Mil-Hdbk-1783)

MIL-STD-879 - Designation Of Aircraft Propulsion Gas Turbine Engines (S/S By Mil-Std-1812)

This standard describes the method, assignment, and arrangement of letters and numerals used by the Military Services in establishing the type and model designation of aircraft propulsion gas turbine engines.