MIL I 23659 : C
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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INITIATOR, ELECTRIC, GENERAL DESIGN SPECIFICATION
03-03-2003
Details general requirements for design and establishes methods for testing electric initiators and subassemblies to determine their electric characteristics, soundness of mechanical design, output, and resistance to deleterious service environments. The term electric initiator includes items classified in FSC 1377 such as hot wire initiators, exploding bridgewire initiators, etc.
DocumentType |
Standard
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Pages |
25
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PublisherName |
US Military Specs/Standards/Handbooks
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Status |
Superseded
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SupersededBy |
MIL-C-82890 Base Document:1993 | CARTRIDGE, FIRE EXTINGUISHER CCU-120/A |
MIL-DTL-32025 Base Document:1998 | CARTRIDGE, IMPULSE, CCU-96/B |
MIL-STD-1399 Revision C:1988 | INTERFACE STANDARD FOR SHIPBOARD SYSTEMS |
MIL-DTL-32027 Base Document:1998 | Generator, Gas, Dry Bay Fire Extinguisher, GGU-15A/A |
MIL-A-82950 Base Document:1995 | ACTUATOR, BELLOWS ATU-117/P |
MIL-D-82687 Base Document:1980 | DEVICE, ARMING FIRING, ROCKET MOTOR MARK 298 MOD O |
MIL-D-81303 Revision A:1966 | DESIGN AND EVALUATION OF CARTRIDGES FOR STORES SUSPENSION EQUIPMENT |
MIL-A-23121 Revision C:1970 | AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-DTL-32106 Base Document:2003 | INITIATORS, ELECTRICAL, FOR ROCKET MOTOR IGNITERS |
DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-D-23615 Revision C:1993 | DESIGN AND EVALUATION OF CARTRIDGE ACTUATED DEVICES |
MIL-HDBK-244 Revision A:1990 | GUIDE TO AIRCRAFT - STORES COMPATIBILITY |
MIL-P-85710 Base Document:1986 | PARACHUTES, PERSONNEL, EMERGENCY ESCAPE GENERAL DESIGN SPECIFICATION FOR |
MIL-C-82894 Base Document:1994 | CARTRIDGE, FIRE EXTINGUISHER, CCU-126/A |
MIL P 87220 : 0 | PROPELLANT, AND EXPLOSIVE SYSTEMS, AIRCRAFT CREW ESCAPE REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT PATTERSON, AFB OH 45433-6503 |
MIL-C-83124 Base Document:1969 | CARTRIDGE ACTUATED DEVICES PROPELLANT ACTUATED DEVICES GENERAL DESIGN SPECIFICATION FOR |
MIL-DTL-81530 Revision B:2000 | Ignition Element, Electric, Mark 11 Mod 0 |
MIL-STD-1901 Revision A:2002 | MUNITION ROCKET AND MISSILE MOTOR IGNITION SYSTEM DESIGN, SAFETY CRITERIA FOR |
MIL-DTL-32022 Base Document:1998 | GENERATOR, GAS, FIRE EXTINGUISHER, GGU-16/A, GGU-17/A, GGU-18/A, GGU-19/A, GGU-20/A |
MIL-I-82877 Base Document:1992 | IGNITION ELEMENT, PVU-15/B |
MIL-A-85317 Base Document:1980 | ACTUATOR, ELECTRO-PYROTECHNIC, LINEAR, ATU-89/B |
MIL-S-18471 Revision G:1983 | System, Aircrew Automated Escape, Ejection Seat Type, General Specification For |
MIL-HDBK-1763 Base Document:1998 | AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
MIL-STD-1399-409 Revision A:1973 | INTERFACE STANDARD FOR SHIPBOARD SYSTEMS SECTION 409 ELECTROMAGNETIC RADIATION HAZARDS TO ORDNANCE |
AOP 39 : 2010 | GUIDANCE ON THE ASSESSMENT AND DEVELOPMENT OF INSENSITIVE MUNITIONS (IM) |
MIL-I-85889 Base Document:1988 | IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
MIL-DTL-82909 Revision A:2003 | Batteries, Thermal, MXU-792A/A and 792B/A |
MIL I 81577 : A | IGNITION ELEMENT, ELECTRIC, MARK 17 MOD 0 |
MIL-P-83126 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
MIL-D-21625 Revision G:1993 | DESIGN AND EVALUATION OF CARTRIDGES FOR CARTRIDGE ACTUATED DEVICES |
MIL-S-23069 Revision A:1983 | SAFETY REQUIREMENTS, MINIMUM, FOR AIR LAUNCHED GUIDED MISSILES |
MIL-STD-322 Revision B:1984 | Explosive Components, Electrically Initiated, Basic Evaluation Tests for |
JSSG-2010-12 Base Document:1998 | Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
MIL-DTL-82939 Base Document:2000 | SEPARATOR, EXPLOSIVE (1W18) |
MIL-DTL-82966 Revision A:2002 | SQUIB, ELECTRIC (DELAY), SQ86 |
MIL-STD-1512 Base Document:1972 | ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS |
MIL I 81530 : A | IGNITION ELEMENT, ELECTRIC MARK 11 MOD O |
FAA AC 20-144 : 0 | RECOMMENDED METHOD FOR FAA APPROVAL OF AIRCRAFT FIRE EXTINGUISHING SYSTEM COMPONENTS |
MIL-STD-1606 Revision A:1983 | TECHNICAL INFORMATION REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE PROPOSALS |
MIL-DTL-81577 Revision B:2000 | Ignition Element, Electric, Mark 17 Mod 0 |
NASA STD 8719.12 : 2010 | SAFETY STANDARD FOR EXPLOSIVES, PROPELLANTS, AND PYROTECHNICS |
MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
MIL-T-60530 Revision A:1971 | TECHNICAL DATA PACKAGE FOR AMC MATERIAL |
MIL-STD-100 Revision G:1997 | ENGINEERING DRAWINGS |
MIL-STD-202 Revision H:2015 | ELECTRONIC AND ELECTRICAL COMPONENT PARTS |
MIL-STD-331 Revision D:2017 | FUZES, IGNITION SAFETY DEVICES AND OTHER RELATED COMPONENTS, ENVIRONMENTAL AND PERFORMANCE TESTS FOR |
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