MIL-STD-1576 Base Document:1984
Current
The latest, up-to-date edition.
ELECTROEXPLOSIVE SUBSYSTEM SAFETY REQUIREMENTS AND TEST METHODS FOR SPACE SYSTEMS
Important note : All end users must be registered with an Account prior to user licenses being assigned.Procedure to safeguard against the hazards resulting from electroexplosive subsystems unintentional initiation or failure to fire. Applies to all space vehicle systems. Coverage includes definitions, bonding, materials compatibility, reliability, human factors, traceability, shielding caps, cables, insulation resistance, electrical isolation, physical separation, monitor circuits, control circuits, hermetic sealing, and firing switches and relays. Also gives diagrams and tables.
| Committee |
FSC SAFT
|
| DocumentType |
Standard
|
| Pages |
152
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| DOD-E-83578 Revision A:1987 | EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) |
| BS EN 14607-6:2004 | Space engineering. Mechanical Pyrotechnics |
| NASA MSFC STD 1800 : 2008 | ELECTROSTATIC DISCHARGE (ESD) CONTROL FOR PROPELLANT AND EXPLOSIVE DEVICES |
| I.S. EN 14607-6:2004 | SPACE ENGINEERING - MECHANICAL - PART 6: PYROTECHNICS |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| NASA HDBK 4001 : 0 | ELECTRICAL GROUNDING ARCHITECTURE FOR UNMANNED SPACECRAFT |
| AOP 39 : 2010 | GUIDANCE ON THE ASSESSMENT AND DEVELOPMENT OF INSENSITIVE MUNITIONS (IM) |
| NASA MSFC SPEC 3635 : 2012 | PYROTECHNIC SYSTEM SPECIFICATION |
| NASA STD 8719.24 : 2011 | NASA EXPENDABLE LAUNCH VEHICLE PAYLOAD SAFETY REQUIREMENTS |
| NASA SPEC 5022:2015 | NASA MANUFACTURING AND TEST REQUIREMENTS FOR NORMALLY CLOSED PYROVALVES FOR HAZARDOUS FLIGHT SYSTEMS APPLICATIONS |
| NASA MSFC SPEC 494 : 2009 | INSTALLATION OF HARNESS ASSEMBLIES (ELECTRICAL WIRING), SPACE VEHICLE, GENERAL SPECIFICATION FOR |
| ISO 26871:2012 | Space systems Explosive systems and devices |
| EN 14607-6:2004 | Space engineering - Mechanical - Part 6: Pyrotechnics |
| FAA AC 20-144 : 0 | RECOMMENDED METHOD FOR FAA APPROVAL OF AIRCRAFT FIRE EXTINGUISHING SYSTEM COMPONENTS |
| NASA STD 5005(INT) : 2007 | THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
| 03/301398 DC : DRAFT JAN 2003 | EN 14607-6 - SPACE ENGINEERING - MECHANICAL - PART 6: PYROTECHNICS |
| SAE USCAR 28 : 2005 | INITIATOR TECHNICAL REQUIREMENTS AND VALIDATION |
| MIL-STD-1546 Revision B:1992 | PARTS, MATERIALS, AND PROCESSES CONTROL PROGRAM FOR SPACE AND LAUNCH VEHICLES |
| FED-STD-228 Revision A:2014 | TEST METHODS FOR CABLES AND WIRE, INSULATED |
| MIL-STD-1168 Revision C:2014 | Ammunition Lot Numbering and Ammunition Data Card |
| MIL-STD-410 Revision E:1991 | NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (EDDY CURRENT, LIQUID PENETRANT, MAGNETIC PARTICLE, RADIOGRAPHIC AND ULTRASONIC) |
| MIL-STD-1547 Revision B:1992 | ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE VEHICLES |
| DOD-E-8983 Revision C:1977 | ELECTRONIC EQUIPMENT, AEROSPACE, EXTENDED SPACE ENVIRONMENT, GENERAL SPECIFICATION FOR |
| MIL-STD-1512 Base Document:1972 | ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS |
| MIL-STD-453 Revision C:1984 | INSPECTION, RADIOGRAPHIC |
| QQ-B-575 Revision C:1993 | BRAID, WIRE, (COPPER, TIN COATED, OR SILVER COATED, TUBULAR, OR FLAT) |
| ASTM E 545 : 2014 : REDLINE | Standard Test Method for Determining Image Quality in Direct Thermal Neutron Radiographic Examination |
| MIL-STD-202 Revision H:2015 | ELECTRONIC AND ELECTRICAL COMPONENT PARTS |
| DOD-E-83578 Revision A:1987 | EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) |
| MIL-STD-1167 Revision C:1985 | AMMUNITION DATA CARD |
| FED-STD-595 Revision C:2008 | COLORS USED IN GOVERNMENT PROCUREMENT |
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