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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
Strength testing and probability calculation
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
Instrumentation of a Tandem Helicopter for Static and Dynamic Stability and Control Flight Tests
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
Observer Program Information Packet 1962 Test Series, DOMINIC
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)
Resonance Tests on a Beagle B206 Series 1 Aircraft
The Design and Testing of an Inflated Sphere Impact Limiter
Physiologic Observations on Race Car Drivers
The Design and Flight Testing of a Take-off and Overshoot Director
A Systematic Method for Determining the Best Altimeter Display for High Performance Aircraft
Advantages of Multipoint Control for Vibration Testing of Complete Ranger Spacecraft
Development of a Long Range Plan for Engineering Research on Flexible Pavements