Spacecraft Attitude Control System, Prototype and Test Final Analysis and Test Report
Performance tests of prototype liquid ammonia spacecraft attitude control systems
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Performance tests of prototype liquid ammonia spacecraft attitude control systems
Thermal cycling machines and accelerated test techniques to improve solder joints for Apollo Telescope Mount
Nickel-200 fatigue testing for thermal fatigue data on regeneratively cooled hypersonic research engine structures
Ideal approaches to accelerated life tests and data analysis applied to space batteries
Postflight test and analysis of parts and material of Surveyor 3 retieved from lunar surface by Apollo 12
Static testing of San Marco 2 satellite and its temperature control system
Proposed dynamic flight testing of Apollo spacecraft
Facility modification plan for testing 260-inch diameter solid rocket engine
Manned spacecraft nonmetallic construction materials selection criteria, testing and configuration control, considering flammability hazard
Development and fabrication of filament composite nondestructive test standards
Effect of radiation on structural materials for NERVA engine tested at cryogenic and elevated temperatures - Vol. 4
Static tests of augmentor-wing flap system for modified C-8A jet STOL research airplane using 0.7 scale model
Development of unified test equipment concept for space shuttle ground support system
Hypervelocity wind tunnel static stability and control tests of variable geometry configuration of space shuttle
Inconel-steel, puddle-welded rotor spin and magnetic testing for use in 36,000 rpm Lundell alternator
Electric-equipment and drive adapter endurance tests for SNAP 8
Service life/stress testing, failure analysis and corrective action from technical and cost positions
A preliminary plan and procedure are presented for conducting an extended manned test program for a regenerative life support system. Emphasis will be placed on elements associated with long-term system operation and long-term uninterrupted crew confinement.