MIL P 87220 : 0
Withdrawn
Withdrawn
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
Publisher
Withdrawn date
03-01-1994
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Describes explosive and propellant systems for aircraft crew escape.
| Committee |
FSC 1377
|
| DocumentType |
Standard
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| MIL-E-87235 Base Document:1985 | Emergency Escape, Aircraft (S/S by AFGS-87235) |
| MIL F 18240 : E | FASTENER ELEMENT, SELF-LOCKING, THREADED FASTENER, 250 DEG F MAXIMUM |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL H 25579 : E | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL I 23659 : C | INITIATOR, ELECTRIC, GENERAL DESIGN SPECIFICATION |
| MIL-STD-1512 Base Document:1972 | ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS (S/S BY MIL-HDBK-1512) |
| MIL-STD-882 Revision E:2012 | System Safety |
| MIL-STD-331 Revision D:2017 | Fuzes, Ignition Safety Devices and Other Related Components, Environmental and Performance Tests for |
Summarise
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