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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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Flight test of 30 foot nominal diameter cross parachute to measure shock loads, drag efficiency, and stability characteristics
Flight test of l0-foot nominal-diameter disk-gap band parachute to determine deployment and inflation, opening shock loads, drag efficiency, and stability characteristics
Maximum drop diameters for atomization of liquid jets injected concurrently into accelerating or decelerating gas streams
Noncavitating and cavitating performance of two low area ratio water jet pumps with throat lengths of 5.66 diameters
Portable electromagnetic coil enables high precision expansion or constriction and joining of large diameter metal tubes. A nonconducting mandrel or forming die is used on the side of the tubes wall opposite the coil. The coil is insulated from the tube by a thin plastic sleeve.
Noncavitating and cavitating performance of low area ratio water jet pumps having throat lengths of 3.54 diameters
Calorimetric evaluation of three 1.5-meter diameter inflatable rigidized solar concentrators for solar dynamic cycle power systems
Design of injectors and ablative thrust chambers for FLOX propane rocket engine with 1.2 inch throat diameter
Research and development of fiber glass filament wound engine case design for 260 inch diameter class solid propellant rocket engines
Half intensity angular diameter upper limit of Seyfert galaxy NGC 4151 nucleus, considering nonthermal continuum
Galactic center observations over various wavelengths including polarization, diameter, flux measurements and power output
Static pressure-diameter measurements on small pulmonary blood vessels of frogs, analyzing capillary septal area as function of intravascular pressures noting high compliance
Radio astronomical studies with 1500 meter diameter low frequency telescope
Gaseous-helium requirements for discharge of liquid hydrogen from 5-ft diameter spherical tank
Diameter, density, and atmospheric data calculated for Neptune from 7 Apr. 1968 occultation
Pressure, subcooling, and diameter effects on film boiling of liquid nitrogen on thin wires
Endurance test of glass coated accelerator grid on 15-centimeter-diameter Kaufman thruster
Facility modification plan for testing 260-inch diameter solid rocket engine