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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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Steady-state pressure drop characteristics of normal hydrogen gas flowing through electrically heated small diameter tube - laminar flow instability
Cooldown of large-diameter liquid hydrogen and liquid oxygen propellant piping systems at M-1 engine test complex
Large diameter self-erecting passive communication satellite
Operation of one-half inch diameter ion thrustor with countercurrent electron accelerator
Explosive sizing of 70-inch diameter welded aluminum preforms and tool design of explosive form die
Relation between diameter of lightning streamer and its radiated radio frequency spectrum
Inflation, drag, and stability characteristics of 26-meter diameter ringsail parachute in simulated Martian environment
Development of 260-inch diameter solid propellant rocket motor
425-foot diameter passive communication satellite with self erecting properties
Adjustable rotor device for generating ellipses over arbitrary pair of conjugate diameters
Flight test of 31.2-foot-diameter modified ringsail parachute deployed at Mach 1.39 and dynamic pressure of 11 pounds per square foot
Division error correction to degree diameters for meridian circle of Odessa Astronomical Observatory
Aerodynamic characteristics of seven foot diameter ducted propeller in wind tunnel
Normal gravity self-pressurization of 9 in. diameter spherical liquid hydrogen tankage
Center-to-limb variations for continuum, faint iron lines and core of strong Fraunhofer lines measured along polar and equatorial diameters of solar disk
Third 260-inch diameter solid propellant rocket engine test firing
Report describes methods for the fabrication of tungsten and tungsten alloys into small-diameter, thin-wall tubing of nuclear quality. The tungsten, or tungsten alloy tube blanks are produced by double extrusion. Plug-drawing has emerged as an excellent secondary fabrication technique for the reduction of the overall tube dimensions.
15-cm diameter, hollow-cathode Kaufman thrustor for SERT 2 mission