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NPFC - MIL-D-8708

DEMONSTRATION: AIRCRAFT WEAPON SYSTEMS, GENERAL SPECIFICATION FOR

inactive
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Organization: NPFC
Publication Date: 31 January 1969
Status: inactive
Page Count: 161

Document History

MIL-D-8708
July 19, 2019
Demonstration: Aircraft Weapon Systems, General Specification for
A description is not available for this item.
MIL-D-8708
August 12, 1991
DEMONSTRATION: AIRCRAFT WEAPON SYSTEMS, GENERAL SPECIFICATION FOR
This specification establishes the general requirements for demonstration of Naval aircraft weapon systems during full scale engineering development. The general requirements may be modified and...
MIL-D-8708
June 3, 1982
DEMONSTRATION: AIRCRAFT WEAPON SYSTEMS, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-D-8708
January 31, 1969
DEMONSTRATION: AIRCRAFT WEAPON SYSTEMS, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-D-8708
September 13, 1960
DEMONSTRATION: AIRCRAFT WEAPON SYSTEMS, GENERAL SPECIFICATION FOR
A description is not available for this item.

References

This document references:
MIL-A-8863 - AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
Published by NPFC on July 19, 1993
This specification defines the strength and rigidity requirements applicable to land-based and ship-based airplanes for the following ground loading conditions: a. Take-offs. b. Landings c. Ground...
This document references:
MIL-A-8870 - Airplane Strength and Rigidity Vibration, Flutter, and Divergence
Published by NPFC on June 11, 2019
A description is not available for this item.
This document references:
MIL-B-85584 - BATTERY RELAY CONTROL UNIT, AIRCRAFT
Published by NPFC on March 27, 1995
This specification covers the requirements for the design, performance, manufacture, and acceptance of a battery relay control unit (BRCU) for use in aircraft to prevent unintentional discharge of...
This document references:
MIL-DTL-85110 - BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENTS FOR
Published by NPFC on September 22, 1997
This specification establishes the requirements for the design, construction, performance, and test of the repeatable release holdback bar (RRHB) for use on carrier-type aircraft.
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