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Phoenix Iron Co.'s two million pound hydraulic
Testing steel for Marine engine construction
Miscellaneous notes on impact tests
Fereday and Palmer's patent stress recorder
Flight Test of Ctv MK 17, MOD 1, No 104-Bendix Autopilot Missile (Ctv-8A17A)
Preliminary Investigation of Fire Bombs for High-Performance Fighter Aircraft
Use of Effectiveness of Shoulder Harness in Surplus Military Aircraft Flown by Civilian Pilots
Aircraft Drops of Mine Parachute, XH-20G, Attached to Mine, Mk. 36
Spin Testing ... United States Navy High Performance Airplanes
Development of an Aircraft Monitor and Control (AMAC) System (RYU-7/A24-DSN-3) for the DSN-3 Drone
Dynamic Test of a Commercial-Type Passenger Seat Installation in an H-21 Helicopter
Preliminary Flight Test Data. Xh-51A Rigid Rotor High Speed Flight Program
Military Potential Test of the Model PA23-250C Fixed-Wing Instrument Trainer
Preliminary Flight Test Data. Xh-51A Rigid Rotor High Speed Flight Program
Snap Aerospace Safety Program. Quarterly Technical Progress Report, October--December 1963
1964 Annual Joint Army-Navy Aircraft Instrumentation Research Progress Report
Voyager Project Progress Report, Oct. 16 - Nov. 15, 1965
The integration of scientific instruments into mariner iv.
The integration of scientific instruments into Mariner IV.
Snap Aerospace Safety Program. Progress Report, April--June 1965
Mariner IV Science Platform Structure and Actuator Design, Development and Flight Performance
Installation and Test of the TCE1-FRG Expeditionary Catapult at the Naval Air Test Facility (Si)
The Design and Testing of an Inflated Sphere Impact Limiter
Physiologic Observations on Race Car Drivers
A Systematic Method for Determining the Best Altimeter Display for High Performance Aircraft
Advantages of Multipoint Control for Vibration Testing of Complete Ranger Spacecraft
Design, Development, Testing and Flight Performance of Mariner MARS Planetary Scan System
C-141a Engineering Flight Test Results of the Aerial Delivery System Tests
Flying Qualities Conference Wright-Patterson Air Force Base, Ohio 5 and 6 April 1966
Theoretical Operating Limitations of the Variable-Stability F-8D
Engineering Flight Test of the UH-1C Helicopter Equipped with the XM-30 Weapon System