MIL-STD-2100 Base Document:1979
Current
Current
The latest, up-to-date edition.
Propellant, Solid, Characterization Of (Except Gun Propellant)
Available format(s)
PDF
Language(s)
English
Published date
30-03-1979
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.| DocumentType |
Standard
|
| Pages |
37
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
The purpose of this standard is to provide a compendium of standardized methods to determine the intrinsic physical, chemical and interface properties of a solid propellant or propellants proposed for use in tactical rockets, missiles, aircrew escape systems, or auxiliary devices.
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| MIL-A-85097-12 Base Document:1984 | AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS); ROCKET CATAPULT MARK 18 MOD 0 (LOADED ASSEMBLY) |
| MIL-A-85097-9 Revision A:1984 | AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS); ROCKET CATAPULT MARK 12 MOD 1 (LOADED ASSEMBLY) |
| MIL-P-83126 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
| MIL A 85097 : B | AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS), PROCUREMENT SPECIFICATION FOR |
| MIL-DTL-85097 Revision E:2000 | USN/USMC PROPELLANT ACTUATED DEVICES (PADS) - GENERAL SPECIFICATION FOR |
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