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Possible Methods of Producing the Gravity-Free State for Medical Research
Service Test of the AN/UAS-4 Infrared Surveillance System Installed in an AO-1C Airplane
Studies Performed to Determine Suspension Needs for Lance Limited Mobility Launcher
The Performance of Fans in Hovercraft. A Method of Reducing Experimental Results
Pressurization System for Use in the APOLLO Service Propulsion System Interim Report
Hybrid Propulsion System for an Advanced Rocket-Powered Target Missile
Airplane Size and Staging Effects on SST Cruise Sonic Boom
Lightweight Small-Frontal-Area Accessory and Drive System Program
Ground Support Equipment Technology Lightweight Launchers for Shoulder-Fired Rockets
A Fuel Tank Inerting System for Military Aircraft. Volume I
SST Parametric Engine Library - Installed Engine Performance
Guenstige Aussichten fuer Verbundwerkstoffe in der Luft- und Raumfahrtindustrie
Power Transfer Systems for Future Navy Helicopters
Influence of Turbine Engine Lubricant Load Carrying Ability on Gear System Design
Light metals offer versatility and strength at a fair price
Radsatzlager mit Leichtmetallgehaeusen fuer die neuen Zuericher Vorort-Triebzuege
Experiment Definition Phase Shuttle Laboratory Ldrl-10.6 Experiment
Truck Noise IV-D: The Reduction of Engine Noise on Heavy Duty Diesel Trucks
Application of Circulation Control Rotor Technology to a Stopped Rotor Aircraft Design
Aluminum radiator bids to succeed where others failed
New sheet molding compounds promise higher strength, easier processing
Research Requirements to Reduce Empty Weight of Helicopters by Use of Advanced Materials
Research Requirements for Development of Regenerative Engines for Helicopters
Conceptual Design Study of 1985 Commercial Tilt Rotor Transports. Volume 3: STOL Design Summary
Concepts for Design of Lightweight Track for the U.S. Marine Landing Vehicle Assault (LVA)
Design and Analysis of Winglets for Military Aircraft
Advanced Design Composite Aircraft (ADCA) Study. Volume 1
Use of high strength steels in the automotive industry to obtain mass reduction