共找到 102 条与 航天用起爆点火装置 相关的标准,共 7 页
This notice should be filed in front of MIL-L-Z2769A(AS), dated 15 January 1962, and Amendment 1, dated 10 November 1983.
LAUNCHER, WEAPONS, AIRBORNE AND ASSOCIATED EQUIPMENT, GENERAL SPECIFICATION FOR
This commercial item description covers brown kraft paper used for general wrapping applications.
LAUNCHER, TRANSPORTER, BRIDGE: M48A5 OR M60A1 TANK CHASSIS
本规范规定了操纵机械引信保险的航空炸弹(以下简称炸弹)的爆炸与不爆炸控制机构(以下简称爆控机构)的设计、研制、生产、交付验收应遵循的一般要求和基本依据。 本规范适用于以抽脱式和剪断式爆控拉杆操纵炸弹引信保险和其它保险的爆控机构。亦适用于其它拉杆操纵炸弹引信保险和其它保险的爆控机构。 本规范的要求与合同(或技术协议)要求不一致时,按合同(或技术协议)要求执行。
General specification for mechanical fuze detonation control mechanism
mis specification is approved for use by all Departments and Agencies of the Department of Defense.
DELAY ELEMENT, CARTRIDGE, M28 ASSEMBLY
This specification covers the cupola body assembly required for the armored vehicle bridge launcher, M60A1 and M48A5 tank chassis.
CUPOLA BODY ASSEMBLY FOR ARMORED VEHICLE BRIDGE LAUNCHER, M60A1 AND M48A5 TANK CHASSIS
This specification covers hydraulic cylinder assemblies for the M48A2, M48A5, and M60A1 bridge launcher-transporters and the hydraulic cylinder assembly for the armored vehicle launched bridge.
MILITARY SPECIFICATION CYLINDER ASSEMBLIES, ACTUATING, LINEAR: HYDRAULIC, FOR BRIDGE AND BRIDGE LAUNCHER
This specification covers requirements for the M69 Cartridge Delay Element (see 6.1).
DELAY ELEMENT, CARTRIDGE, M69 ASSEMBLY
This specification covers the requirements for the M13 Cartridge Delay Element (see 6.1).
DELAY ELEMENT, CARTRIDGE, M13 ASSEMBLY
MIL-I-23951(AS) (l), dated 1 September 1966, has been reviewed and determined to be valid for use in acquisition.
IGNITION MATERIAL, PELLETED, PYROTECHNIC
This specification covers the requirements for the M8 Cartridge Delay Element (see6.i).
DELAY ELEMENT, CARTRIDGE, M8 ASSEMBLY
The launcher shall provide for the carriage, service and power e j e c t i o n release of an airborne guided m i s s i l e w i the i the r a nuclear or conventional warhead from t a c t i c a l a i r c r a f t i n f l i g h t .
LAUNCHER, EJECTION, GUIDED MISSILE AIRCRAFT, GENERAL DESIGN CRITERIA FOR
DELAY ELEMENT, CARTRIDGE, M5 ASSEMBLY
DELAY ELEMENT, CARTRIDGE, M5 ASSEMBLY
This specification establishes the requirements for the manufacture and inspection o f the Launcher, Rocket LMU-24A/E and LMU-24BIE.
LAUNCHER, ROCKET LMU-24A/E AND LMU-24B/E
This specification i s approved for use by the Naval A i r Systems Command, Department o f the Navy, and i s available for use by all Departments and Agencies o f the Department of Defense. 1. SCOPE 1.1 Scope. This specification
IGNITER, PVU-3A/E AND PVU-3B/E
This specification i s approved for use by the Naval A i r Systems Command, Department o f the Navy, and i s available for use by all Departments and Agencies of the Department o f Defense.
LAUNCHER, ROCKET LMU-23A/E AND LMU-23B/E
This standard establishes the. format, contents , and ppocedures fop the preparation of depot PewoFk
DEPOT REWORK SPECIFICATION, AIR-LAUNCHED WEAPONS, ARMAMENT, ORDNANCE, MISSILE LAUNCHERS, AND PECULIAR SUPPORT EQUIPMENT, PREPARATION OF [Superseded: SAI AS 2177.1]
To establish recommended gap settings for aircraft piston engine spark plugs. To standardize gap settings for spark plugs for commercial applications for all types of aircraft piston engines.
Gap Settings for Aircraft Piston Engine Spark Plugs
MIi-I-23488(Nep) dated 19 October 1962, and Amendment 1, dated 7 December 1964, have been reviewed and determined to be still current.
IGNITION ELEMENT, ELECTRIC, MARK 10 MOD 6
This amendment forms a part of Military Specification MIL-C-60842(MU), dated 8 December.1970, 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.
DELAY ELEMENT, CARTRIDGE, XM17 ASSEMBLY
This specification covers reciprocating engine shielded and unshielded spark plugs.
Spark Plugs, Aircraft Engine
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