MIL-C-27410 - Components, Rocket Propulsion Fluid System, General Specification For
This specification covers the requirements and instructions for preparation of the manufacturer's model specification for all components of a rocket propulsion system which control the pressure or flow of ullage, gas, pressurizing gas, propellants, combustion products, or hydraulic fluid.
MIL-E-19042 - Engine, Rocket, Solid Propellant, 2.2 Second Duration - 11,000 Pounds Thrust
MIL-E-19043 - Engine, Rocket, Solid Propellant, 2.2 Second Duration, 33,000 Pounds Thrust
MIL-E-25277 - Engine, Rocket, Dummy, Type Mf-1
MIL-E-5150 - Engine, Rocket, Liquid Propellant, Model Specification For, Outline And Instructions For Preparation Of (S/S By Mil-R-5149)
MIL-E-5151 - Engine, Rocket, Liquid Propellant, Qualification Test For (S/S By Mil-R-5149)
MIL-E-5152 - Engine, Rocket, Liquid Propellant, Acceptance Test For (S/S By Mil-R-5149)
MIL-E-6626 - Engines, Rocket, Liquid Propellant, Preliminary Flight Rating Test For (S/S By Mil-R-5149)
MIL-E-8581 - (
Images) Engine, Rocket, Solid Propellant, 5 Second Duration, 4500 Pounds Thrust (S/S By Sae-As8581)
This specification established the requirements for a 5 second duration, 4500 pound thrust (when determined at 60 deg. F) solid propellant rocket engine hereinafter specified as 5 S-4500.
MIL-J-8667 - Jet Assisted Take Off Systems - Design And Installation Of, In Naval Aircraft
This specification establishes the requirements for the design, installation, test and data requirements for Jet Assisted Take-off Systems for Naval aircraft.
MIL-P-25413 - Power Unit, Liquid Propellant, General Specification For
MIL-P-25414 - Power Unit, Liquid Propellant, Model Specification For, Outline And Instructions For Preparation Of
MIL-P-25415 - Power Unit, Liquid Propellant, Qualification Test For
MIL-P-25416 - Power Unit, Liquid Propellant, Acceptance Test For
MIL-P-25417 - Power Unit, Liquid Propellant Preliminary Flight Rating Test For
MIL-P-27409 - Propellant Feed System, Rocket Propulsion, General Specification For
This specification covers the propellant feed system consisting of the vehicle portion of the propulsion system and includes the propellant and pressurant tankage, all components such as the valves, regulators and switches, the lines and fittings, the propellant gaging and utilization system, the propellant orientation device or system, the vent and relief system, the servicing system, and other items needed to supply propellants to the rocket engine at the proper pressure, temperature, flow rate and mixture ratio.
MIL-R-5149 - Rocket Engine, Liquid Propellant, General Specification For
This specification covers standard requirements for a liquid propellant rocket engine (6.3.35) and includes the requirements for the outline and instructions for the preparation of the manufacturer's engine model specification (appendix).
MIL-R-6124 - Rocket Engine, Liquid Propellant, Preparation For Storage & Shipment Of
MIL-STD-815 - Type Designation System For Rocket Engines, Motors And Hybrids (S/S By Mil-Std-1812)
The purpose of this standard is to provide a uniform type designation system for use by the Department of the Air Force in identifying a rocket engine, motor, cluster and hybrid ; hereinafter referred to as propulsion devices.
MIL-T-5208 - Tank, Removable, Liquid Propellant Rocket Engine, General Specification For
This specification covers the general requirements for removable tanks for liquid propellant rocket engine systems.
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