资料描述
MIL-PRF-38534G, PERFORMANCE SPECIFICATION: HYBRID MICROCIRCUITS, GENERAL SPECIFICATION FOR (9 MAR 2009)., This specification establishes the general performance requirements for hybrid microcircuits, multi- chip modules (MCM) and similar devices, and the verification requirements for ensuring that these devices meet the applicable performance requirements. Verification is accomplished through the use of one of two quality programs (Appendix A). The main body of this specification describes the performance requirements and the requirements for obtaining a Qualified Manufacturers List (QML) listing. The appendices of this specification are intended for guidance to aid a manufacturer in developing their verification program. Detail requirements, specific characteristics, and other provisions that are sensitive to the particular intended use should be specified in the applicable device acquisition specification.
MIL-PRF-38534F
MIL-PRF-38534F, PERFORMANCE SPECIFICATION: HYBRID MICROCIRCUITS, GENERAL SPECIFICATION FOR (12 APR 2006)., This specification establishes the general performance requirements for hybrid microcircuits, Multi- Chip Modules (MCM) and, similar devices and the
MIL-PRF-38534E
MIL-PRF-38534E, PERFORMANCE SPECIFICATION: HYBRID MICROCIRCUITS, GENERAL SPECIFICATION FOR (6 JAN 2003)., This specification establishes the general performance requirements for hybrid microcircuits, Multi- Chip Modules (MCM) and similar devices and the v
MIL-PRF-38534D
MIL-PRF-38534D, PERFORMANCE SPECIFICATION: HYBRID MICROCIRCUITS, GENERAL SPECIFICATION FOR (6 JAN 1999). This specification establishes the general performance requirements for hybrid microcircuits, Multi-Chip Modules (MCM) and similar devices and the ver
MIL-PRF-38413D (NOTICE 1)
MIL-PRF-38413D (NOTICE 1), PERFORMANCE SPECIFICATION TECHNICAL MANUAL AND FLIGHT CREW CHECKLISTS FOR AIR REFUELING PROCEDURES (1 MAR 1996) [SUPERSEDING MIL-M-38413C] [S/S BY MIL-DTL-7700G]., MIL-PRF-38413D(USAF), dated 1 Mar 1996, which has been wholly in
MIL-PRF-38413D
MIL-PRF-38413D, PERFORMANCE SPECIFICATION TECHNICAL MANUAL AND FLIGHT CREW CHECKLISTS FOR AIR REFUELING PROCEDURES (1 MAR 1996) [SUPERSEDING MIL-M-38413C]., This specification covers the preparation of air refueling procedures flight manuals and checklist
MIL-PRF-38314 (USAF)
MIL-PRF-38314 (USAF), PERFORMANCE SPECIFICATION MANUALS, TECHNICAL: OPERATION AND ASSOCIATED CHECKLIST (SPACE SYSTEMS), PREPARATION OF (18 AUG 1997)., This specification covers requirements for the preparation of operation manuals and associated checklist
MIL-PRF-38311C
MIL-PRF-38311C, PERFORMANCE SPECIFICATION MANUALS, TECHNICAL: OPERATION AND ASSOCIATED CHECKLIST (INTERCONTINENTAL BALLISTIC MISSILE) PREPARATION OF (9 DEC 1997) [SUPERSEDING MIL-M-38311B].,
MIL-PRF-38219C (AMENDMENT 1)
MIL-PRF-38219C (AMENDMENT 1), PERFORMANCE SPECIFICATION: TURBINE FUEL, LOW VOLATILITY, JP-7 (03 OCT 1997) [SUPERSEDING MIL-T-38218B]., This amendment forms a part of MIL-PRF-38219C, dated 18 September 1995, and is approved for use by the Department of the
MIL-PRF-38219C
MIL-PRF-38219C, PERFORMANCE SPECIFICATION: TURBINE FUEL, LOW VOLATILITY, JP-7 (18 SEP 1995) [SUPERSEDING MIL-T-38218B]., This specification covers one grade of aviation turbine fuel designated as JP-7.
MIL-PRF-38169A
MIL-PRF-38169A, PERFORMANCE SPECIFICATION: LENS, GOGGLE AND VISOR, HELMET, OPTICAL CHARACTERISTICS, GENERAL SPECIFICATION FOR (10 JUN 1998) [SUPERSEDING MIL-L-38169]., This is a general specification for optical characteristics of helmet visor and goggle
MIL-PRF-38039
MIL-PRF-38039, PERFORMANCE SPECIFICATION: SYSTEMS, ILLUMINATED, WARNING, CAUTION, AND ADVISORY, GENERAL SPECIFICATION FOR (11 MAY 1998) [SUPERSEDING MIL-S-38039B]., This specification covers the general requirements for illuminated warning, caution, and a
MIL-PRF-32327
MIL-PRF-32327, PERFORMANCE SPECIFICATION: RIFLE, CALIBER .50; SNIPER W/DAY OPTIC SIGHT AND CARRYING CASES - M107 (20 MAR 2009)., This specification prescribes the performance requirements and identifies the verification procedures for the RIFLE: caliber .
MIL-PRF-32317
MIL-PRF-32317, PERFORMANCE SPECIFICATION: CARTRIDGE, 7.62MM: ARMOR PIERCING - M993 (10 MAR 2009)., This specification describes the performance requirements and verification methods for the Cartridge, 7.62MM: armor piercing, M993 for use in 7.62MM weapons
MIL-PRF-32316 (W/AMENDMENT 1)
MIL-PRF-32316 (W/AMENDMENT 1), PERFORMANCE SPECIFICATION: RIFLE, 7.62MM; SEMI-AUTOMATIC SNIPER SYSTEM (SASS) - M110 (05 OCT 2009)., This specification defines the technical and performance requirements, and the associated quality assurance provisions and
MIL-PRF-32316
MIL-PRF-32316, PERFORMANCE SPECIFICATION: RIFLE, 7.62MM; SEMI-AUTOMATIC SNIPER SYSTEM (SASS) - M110 (07 OCT 2008)., This specification defines the technical and performance requirements, and the associated quality assurance provisions and verification pro
MIL-PRF-32300
MIL-PRF-32300, PERFORMANCE SPECIFICATION: CARTRIDGE, 12 GAGE SHOTGUN: BREACHING - M1030 (28 JUL 2008)., This specification identifies the performance requirements and verification provisions for the CARTRIDGE, 12 GAGE SHOTGUN: breaching, M1030 for one-sho
MIL-PRF-32273
MIL-PRF-32273, PERFORMANCE SPECIFICATION: BATTERY CELLS AND MODULES, VALVE REGULATED LEAD-ACID, MAIN STORAGE, SUBMARINE; GENERAL SPECIFICATION FOR (31 OCT 2007)., This specification covers valve regulated lead-acid (VRLA) main storage battery cells (see 6
MIL-PRF-32272
MIL-PRF-32272, PERFORMANCE SPECIFICATION: INTEGRATED POWER NODE CENTER (IPNC) (29 OCT 2007)., This specification covers the Integrated Power Node Center (IPNC), herein referred to as the IPNC. The IPNC can provide distribution, switching, control, and con
MIL-PRF-32269
MIL-PRF-32269, PERFORMANCE SPECIFICATION, PERFORATED HOMOGENEOUS STEEL ARMOR (18 OCT 2007)., This specification covers perforated homogeneous steel appliqué armor in nominal thicknesses from 0. 250 - 2.000 inch, inclusive.
MIL-PRF-32239
MIL-PRF-32239, PERFORMANCE SPECIFICATION, COATING SYSTEM, ADVANCED PERFORMANCE, FOR AEROSPACE APPLICATIONS. This specification establishes the requirements for coating systems having high durability to be used in finishing aircraft exterior surfaces. Thes