MIL-PRF-24751A

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MIL-PRF-24751A, PERFORMANCE SPECIFICATION, FANS, VANEAXIAL GAS TURBINE ENCLOSURE COOLING NAVAL SHIPBOARD (16 DEC 2004) [SUPERSEDING MIL-F-24751]., This specification covers high pressure and HI shock, type TA vaneaxial fans for use in cooling the gas turbine enclosures of ship propulsion/generator systems.


MIL-PRF-24751A
MIL-PRF-24751A, PERFORMANCE SPECIFICATION, FANS, VANEAXIAL GAS TURBINE ENCLOSURE COOLING NAVAL SHIPBOARD (16 DEC 2004) [SUPERSEDING MIL-F-24751]., This specification covers high pressure and HI shock, type TA vaneaxial fans for use in cooling the gas turbine enclosures of ship propulsion/generator systems.

MIL-PRF-24758A (SH)
MIL-PRF-24758A (SH), PERFORMANCE SPECIFICATION CONDUIT SYSTEMS, FLEXIBLE, WEATHERPROOF (24 SEP 2004)., This specification covers the performance requirements for weatherproof flexible conduit systems (see 6.3.12) for use primarily in exposed areas (see 6.3.10) on U.S. Navy ships, to shield against electromagnetic (EM) radiation from own-ship transmitters and emissions external to the ship, electromagnetic pulse (EMP) (see 6.3.8) events, and to minimize corrosion (see 6.3.6) while being field repairable to reduce maintenance.

MIL-PRF-25435C
MIL-PRF-25435C, PERFORMANCE SPECIFICATION: TRANSMITTERS, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR (1 APR 1997) [SUPERSEDING MIL-T-25435B]., This specification covers the general requirements for aircraft pressure transmitters.

MIL-PRF-25435D
MIL-PRF-25435D, PERFORMANCE SPECIFICATION: TRANSMITTERS, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR (3 JUL 2008) [SUPERSEDING MIL-T-25435B]., This specification covers the general requirements for aircraft pressure transmitters.

MIL-PRF-25478C
MIL-PRF-25478C, PERFORMANCE SPECIFICATION: COOLERS, LUBRICATING OIL, AIRCRAFT, GENERAL SPECIFICATION FOR (29 DEC 1997) {SUPERSEDING MIL-C-25478B]., This is the general specification for aircraft engine lubricating oil coolers that provide oil temperature regulation for aircraft gas turbine engines using high temperature synthetic base lubricating oil, and aircraft piston engines, turbo propeller gear boxes, and helicopter transmission gear boxes using petroleum based oil.

MIL-PRF-25508F
MIL-PRF-25508F, PERFORMANCE SPECIFICATION, PROPELLANT, OXYGEN (19 OCT 1995) [SUPERSEDING MIL-P-25508E]., This specification covers the requirements for three grades and two types of oxygen.

MIL-PRF-25508G
MIL-PRF-25508G, PERFORMANCE SPECIFICATION, PROPELLANT, OXYGEN (21 NOV 2006) [SUPERSEDING MIL-P-25508E]., This specification covers the requirements for three grades and two types of oxygen.

MIL-PRF-25567E
MIL-PRF-25567E, PERFORMANCE SPECIFICATION, LEAK DETECTION COMPOUND, OXYGEN SYSTEMS (8 JUL 2005)., This specification covers two types of a gas leak detection compound that is compatible with oxygen. The leak detection compound is intended for use in detecting leaks in both high- and low-pressure oxygens systems in aircraft and other related oxygen systems.

MIL-PRF-25567E (NOTICE 1)
MIL-PRF-25567E (NOTICE 1), PERFORMANCE SPECIFICATION, LEAK DETECTION COMPOUND, OXYGEN SYSTEMS (8 JUL 2005)., MIL-PRF-25567E, dated 17 November 1998, has been reviewed and determined to be valid for use in acquisition.

MIL-PRF-25604E
MIL-PRF-25604E, PERFORMANCE SPECIFICATION, PROPELLANT, uns-DIMETHYLHYDRAZINE (1 OCT 1997) [SUPERSEDING MIL-P-25604D]., This specification covers the requirements for unsymmetrical dimethylhydrazine (CH3)2NNH2 propellant (UDMH).

MIL-PRF-25675C
MIL-PRF-25675C, PERFORMANCE SPECIFICATION: VALVES, CHECK, MINIATURE, HYDRAULIC, AIRCRAFT AND MISSILE (26 NOV 1997) [SUPERSEDES MIL-V-25675B, MS24423C AND MS24593D]., This specification covers hydraulic, spring-loaded, normally closed aircraft and missile hydraulic system check valves with operating pressures up to 3,000 pounds per square inch (psi) and operating temperatures from -65 deg to 450 deg F.

MIL-PRF-25675C (AMENDMENT 1)
MIL-PRF-25675C (AMENDMENT 1), PERFORMANCE SPECIFICATION: VALVES, CHECK, MINIATURE, HYDRAULIC, AIRCRAFT AND MISSILE (12 SEP 2002) [SUPERSEDES MIL-V-25675B, MS24423C AND MS24593D]., This amendment forms a part of, MIL-PRF-25675C dated, 26 November 1997 and is approved for use by all Departments and Agencies of the Department of Defense.

MIL-PRF-25676E
MIL-PRF-25676E, PERFORMANCE SPECIFICATION: ADAPTER, PRESSURE LUBRICATING OIL SERVICING, AIRCRAFT (5 MAY 1997) [SUPERSEDING MIL-A-25676D] [S/S BY MIL-DTL-25677]., This specification covers an adapter installed in an aircraft turbine engine lubricating oil system as a connection for ground servicing with pressure lubricating oil servicing equipment, using synthetic lubricating and preservative oil.

MIL-PRF-25676E (NOTICE 1)
MIL-PRF-25676E (NOTICE 1), PERFORMANCE SPECIFICATION: ADAPTER, PRESSURE LUBRICATING OIL SERVICING, AIRCRAFT (11 DEC 1998) [SUPERSEDING MIL-A-25676D] [S/S BY MIL-DTL-25677]., This specification covers an adapter installed in an aircraft turbine engine lubricating oil system as a connection for ground servicing with pressure lubricating oil servicing equipment, using synthetic lubricating and preservative oil.

MIL-PRF-25690B (AMENDMENT 1)
MIL-PRF-25690B (AMENDMENT 1), PERFORMANCE SPECIFICATION PLASTIC, SHEETS, AND FORMED PARTS, MODIFIED ACRYLIC BASE, MONOLITHIC, CRACK PROPAGATION RESISTANT (27 JUN 1995).

MIL-PRF-25962E
MIL-PRF-25962E, PERFORMANCE SPECIFICATION, VALVE, LIQUID OXYGEN DRAIN (15 JAN 2008., This specification covers one type of valve for draining 70 and 300 pounds per square inch gage (psig) liquid oxygen converters.

MIL-PRF-26536E
MIL-PRF-26536E, PERFORMANCE SPECIFICATI0N, PROPELLANT, HYDRAZINE (24 SEP 1997) [SUPERSEDING MIL-P-26536D]., This specification covers the requirements for three grades of hydrazine (N2H4).

MIL-PRF-26536E (AMENDMENT 1)
MIL-PRF-26536E (AMENDMENT 1), PERFORMANCE SPECIFICATI0N, PROPELLANT, HYDRAZINE (24 SEP 1997) [SUPERSEDING MIL-P-26536D]., This amendment forms a part of MIL-PRF-26536E, dated 24 September 1997, and is approved for use by the Departments and Agencies of the Department of Defense.

MIL-PRF-26539E
MIL-PRF-26539E, PERFORMANCE SPECIFICATION: PROPELLANTS, DINITROGEN TETROXIDE (7 OCT 1997) [SUPERSEDING MIL-P-26539D]., This specification covers the requirements for five types and two grades of dinitrogen tetroxide (N2O4) propellants.

MIL-PRF-26539F
MIL-PRF-26539F, PERFORMANCE SPECIFICATION: PROPELLANTS, DINITROGEN TETROXIDE (17 APR 2006)., This specification covers the requirements for all types of dinitrogen tetroxide (N2O4) propellants.



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