A study of the boundary flow in a rocket combustion chamber. Part 3 - Data report Final report
Rocket motor boundary flow sampling apparatus
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Rocket motor boundary flow sampling apparatus
Mission and systems analyses for solar electric propulsion spacecraft flight to asteroid belt - Vol. 1
Design and fabrication of conical wheels for lunar surface vehicle
Ben Franklin submersible use as space station analog
Passive instrumentation and stimuli generation for Saturn IB equipment checkout - nondestructive testing
Chemical composition and mechanical properties of nickel maraging steel plate, forged, and weld wire materials for 260 inch diameter motor chamber and nozzle shell
Summary of Voyager spacecraft systems analysis and engineering tasks
Experiment designs for collecting human factors engineering data on advanced space systems maintenance
Neutral buoyancy simulation of zero gravity conditions encountered in space maintenance and repair
Astronaut EVA and IVA zero gravity performance
Two meter system for large telescope experiment program - summary
Apollo materials toxicity screening tests and effects of ethylene glycol, monomethylhydrazine, NF3, OF2, and ClF3
This final report describes the work that was done to determine the state-of-the-art of valves required for space exploration vehicles and the steps that were taken to advance the technology. Interviews were held with personnel of major prime manufacturers to determine current problems and current and future requirements. Manufacturers were surveyed by mail to determine what equipment is presently being produced. An extensive search of patent office files was made to determine if any novel valve concepts not already applied to aerospace valves might exist. A literature search was conducted to provide the necessary technical information that was required for the program. Several extensive studies were made to determine the effects on materials resulting from use in space applications, and an investigation of the basic phenomena of valve seat wear was initiated. With the information developed in the surveys and studies, the significant problems associated with valves were identified and are described under "Discussion of Problems. " A novel valve concept was developed and a prototype valve was built and successfully tested. A seal compound of Teflon and stainless steel was developed which possesses superior cold flow characteristics while retaining the desirable properties of the basic Teflon material.
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Deep space instrumentation facility /dsif/ spacecraft tracking performance during ranger iv lunar probe mission
Analysis of Deep Space Instrumentation Facility tracking performance during Ranger VII mission
Computer printouts of numerous scientific experiments conducted in mission support for extended lunar exploration
Development of R-4D rocket engine