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标题描述
MIL-A-8869
Airplane Strength and Rigidity Nuclear Weapons Effects
MIL-A-8892
Airplane Strength and Rigidity, Vibration (for Future Procure. (See MIL-A-87221)
MIL-A-8421
Air Transportability Requirements, General Specification for (Future Acquisition use MIL-STD-1791)
AFGS-87237
Navigation Equipment, Airborne (NO S/S Document)
MIL-A-8893
Airplane Strength and Rigidity, Sonic Fatigue (for Future Procure. (See MIL-A-87221)
MIL-HDBK-2066
Catapulting and Arresting Gear Forcing Functions for Aircraft Structural Design
MIL-F-83691
Flight Test Demonstration Requirements for Departure Resistance and Post-Departure Characteristics of Piloted Airplanes (No S/S Document)
MIL-STD-2066
CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN (S/S BY MIL-HDBK-2066)
MIL-STD-1793
FLIGHT PERFORMANCE, A1R VEHICLE (S/S BY MIL-HDBK-1793)
MS33576
DIMENSION, BASIC, COCKPIT, WHEEL CONTROLLED, FIXED WING AIRCRAFT (USE MIL-STD1333 FOR ARMY & NAVY AND DH2-2 FOR AIR FORCE)
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