共找到 444 条与 航天器综合 相关的标准,共 30 页
This description covers a pocket-type microscope with an optical system of between 40X and 60X magnification intended for use in the inspection of scribed lines made on scribed, coated plastic sheets in the color-separation drafting phase of military cartography.
MICROSCOPE, OPTICAL: MONOCULAR, FIXED-FOCUS, POCKET-TYPE, BETWEEN 40X AND 60X MAGNIFICATION
System Design Considerations for Aircraft Electrical Power
System Design Considerations for Aircraft Electrical Power
Aircraft Electrical Power Component Design
Aircraft Electrical Power Component Design
Design Guidance for Aircraft Electrical Power Systems
Design Guidance for Aircraft Electrical Power Systems
Aircraft Electrical Power Utilizing Equipment Design
Aircraft Electrical Power Utilizing Equipment Design
Aircraft Electrical Power Distribution, Protection and Control Charactertics
Aircraft Electrical Power Distribution, Protection and Control Charactertics
This amendment forms a part of Military Specification MIL-S-25948J, dated 17--January 1984 and is-approved for-use by all Depar-tnients and Agencies of the Departanent of Defense.
SUNGLASSES, HGU - 4P (WITH CASE)
This amendment forms a part of Military Specification MIL-R-l4801(MU),dated 7 May 1968, and is approved for use within the Naval Sea Systems Command, Department of the Navy, and is available for use by all Departments and Agencies of the Department of Defense.
REMOVER, AIRCRAFT CANOPY, P/N 2218-18 OVERHAUL OF
This amendment forms a part of Military Specification MIL-H-60648(MU), dated 17 March 1967, and is approved for use within the Naval Sea Systems Command, Department of the Navy, and is available for use by all Departments and Agencies of the Department o f Defense.
HOLDER, STRIP, LOADED, ASSEMBLY MB, M9, M10, XM12, M19 OR XM25 AIRCRAFT EJECTION SEAT CATAPULT
MIL-R-50729A(MU), dated 14 November 1972, has been reviewed and determined t o be current.
REMOVE, AIRCRAFT CANOPY, M8A1 REMANUFACTURED METAL PARTS ASSEMBLY
MIL-E-49383 dated 16 June 1980, has been reviewed and determined to be valid for use in acquisition.
EYEPIECE, BINOCULAR, AN/VSG-2
This specification covers requirements for design and establishes a uniform method of testing one type of Simulator , Launching, Anti-Tank, Guided Missile and Rocket,M22. The purpose of the M22 Simulator testing program is to determine performance, safety,soundness of mechanical design and resistance to environments encountered during storage,handling,and service use.
SIMULATOR, LAUNCHING, ANTI-TANK GUIDED MISSILE AND ROCKET, M22, PERFORMANCE SPECIFICATION FOR
This document covers two types of goggles for wear with and without glasses.
GOGGLES, SUN, WIND AND DUST: 1974 [Use In Lieu Of: DLA MIL-G-0043914 E CANC NOTICE 1]
Verification Regulations for Beat Frequency Oscillators
이 규격은 비행기의 비행하중조건에 대한 강도 및 강성상의 요구사항에 관하여 규정한다.
Airplane Strength and Rigidity, Flight Loads
이 규격은 항공기의 중량구분과 그 구분에 포함되는 내용에 대하여 규정한다.
Weight Distribution of Aircraft
이 규격은 비행기의 착륙 및 지상 취급하중에 대한 강도 및 요구사항에 대하여 규정한다.
Airplane Strength and Rigidity, Landing and Ground Handling Loads
This amendment forms a part of Military Specification MIL-G-635C dated 4 June 1970, and is approve& for use by all Departments and Agencies of the Department of Defense.
GOGGLES, SUN, WIND AND DUST
This specification is approved for use by all Departments and Agencies of the Department of Defense,
SUNGLASSES, HGU - 4P (WITH CASE)
This amendment forms a part of Military Specification MIL-D-23222A, dated 18 March 1971, and is approved for use by the Naval Air Systems Command, Department of the Navy and is available for use by all Departments and Agencies of the Department of
DEMONSTRATION REQUIREMENTS FOR HELICOPTERS
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