NPFC - MIL-DTL-85097/15
AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS); ROCKET MOTOR, MARK 121 MOD 0
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| Organization: | NPFC |
| Publication Date: | 28 November 2005 |
| Status: | active |
| Page Count: | 5 |
scope:
This specification sheet covers requirements unique to the Mark 121 Mod 0 Rocket Motor (see 6.1).
intended Use:
The rocket motor is intended to insure proper trajectory divergence of the aircrew during an escape for the TAV-8B Aircraft Escape System. The rocket motor was designed specifically for use with... View More
Document History
MIL-DTL-85097/15
November 28, 2005
AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS); ROCKET MOTOR, MARK 121 MOD 0
The rocket motor is intended to insure proper trajectory divergence of the aircrew during an escape for the TAV-8B Aircraft Escape System. The rocket motor was designed specifically for use with the...
September 26, 1991
AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS); ROCKET MOTOR, MARK 121 MOD 0
A description is not available for this item.
May 27, 1987
AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS); ROCKET MOTOR, MARK 121 MOD 0
The rocket motor is intended to insure proper trajectory divergence of the aircrew during an escape for the TAV-8B Aircraft Escape System.
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