Radiative attachment of electrons to atomic hydrogen
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Close-tolerance elliptical cones are fabricated by cutting-tool guide assembly used with conventional tracer cartridge on turret lathe accurately produced in two machine operations.
Pressurized steel or aluminum cylindrical shells reinforced by rings and stringers analyzed statically for dynamic response to concentrated radial loads, noting application to Saturn S-IC VEHICLE
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Zero reaction tools require no force application by workers in space. The tool accomplishes hole cutting by holding the workpiece and feeding the cutting blade into and through it by forces entirely absorbed within the tool.
Electron capture detector parameters in pulse sampling mode analyzed, noting kinetic processes, temperature effect, etc
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Approximation of ramjet exhaust plume effects on external pressure of nozzle extension of X-15 aircraft
Inflatable conical shell afterbody ballute for aerodynamic brakes in Mars atmospheric entry
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Crystalline absorption of polymer single crystals
Navigational device, invented to aid recovery of spacecraft from any orbit, also illustrates motions of satellites relative to earth and their entry-ranging requirements. Device rapidly and accurately defines lateral range requirements for spacecraft returning to any desired site without manual or computerized calculation of orbital equations of motion.
Quick-release coupling for fueling rocket vehicles with cryogenic propellants
Principal investigator requirements for lunar module-borne cosmic ray detector experiment
Support requirements for lunar module-borne cosmic ray detector experiment
Reliability requirements for lunar module-borne cosmic ray detector experiment
Television-type, out-window visual simulation image generator design and specifications for aircraft or spacecraft manned flight simulation
Experimental investigation on effect of spot welded or adhesively bonded thermocouples and fatigue behavior of two titanium alloys suitable for use in high speed airplanes