FORTRAN programs for the design of liquid-to-liquid jet pumps
One dimensional equations describing noncavitating and cavitating flow in liquid-to-liquid jet pumps programmed for computer use
Sanger, N. L.↗
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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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Experimental evaluation of a pump test facility with controlled perturbations of inlet flow
Development of facility for experimental evaluation of centrifugal pump operating under periodic fluctuations of inlet pressure and flow
Stevans, W.↗
Evaluation of SNAP-8 liquid NaK pump-motor (NaK PMA) following vibration and shock testing
Vibration and shock testing of SNAP 8 liquid NaK pump motor assembly
Nelson, R. B.↗
An economical and demountable diffusion-pump cold trap
Liquid nitrogen cold trap for oil diffusion pump
Ziniker, W. M.↗
Nuclear pumped gas lasers
Gas lasers pumping by nuclear energy, discussing heavy particle interactions, threshold densities, population inversion, etc
Schneider, R. T.↗
Pump linewidth requirement for optical parametric oscillators
Singly resonant optical parametric oscillator allowable pump bandwidth
Harris, S. E.↗
Pumping mechanism of CO2 laser and formation rate of CO2 from CO and O
Time delay in pulsed optical carbon dioxide laser pumping mechanism in high current gaseous discharge
Chen, C. J.↗
Integrated parametric amplifier module with self-contained solid-state pump source
Integrated S band microstrip parametric amplifier modules with self contained Gunn effect pump oscillator for space flight applications
Allen, C. M.↗
Boiler feed EM pump for a Rankine cycle space power system
Helical induction boiler feed electromagnetic pump design, fabrication and testing for potassium Rankine cycle space power system
Couch, J. P.↗
Spectral absorption of vacuum-pump fluids
Vacuum pump fluids spectral absorption coefficient measurement, using variable UV cell
Gillis, H. L.↗
An adsorption pumped He 3 cooled IR detector
Adsorption cryopumped He 3 cooled IR detector without encumbrance of external diffusion or mechanical pump
Martin, T. Z.↗
Possibility of a unidirectional laser amplifier produced by monochromatic optical pumping of a coupled Doppler-broadened transition
Unidirectional gas laser amplifier using monochromatic optical pumping of coupled Doppler broadened transition
Feld, M. S.↗
Improved method for reclaiming vacuum diffusion pump oil
High vacuum centrifugal molecular distillation system rapidly reclaims contaminated diffusion pump oil in continuous operation and restores it to high level of purity.
Buggele, A. E.↗
Computer programs for the design of liquid-to-liquid jet pumps
Computer programs based on one-dimensional equations for cavitating and noncavitating flow in liquid-to-liquid jet pumps are described.
Sanger, N. L.↗
Optimization of fluid line sizes with pumping power penalty IBM-360 computer program
Computer program has been developed to calculate and total weights for tubing, fluid in tubing, and weight of fuel cell power source necessary to power pump based on flow rate and pressure drop. Program can be used for fluid systems used in any type of aircraft, spacecraft, trucks, ships, refineries, and chemical processing plants.
Jelinek, D.↗
Thermal-powered reciprocating pump
Waste heat from radioisotope thermal generators in spacecraft is transported to keep instruments warm by two-cylinder reciprocating pump powered by energy from warm heat exchange fluid. Each cylinder has thermally nonconductive piston, heat exchange coil, and heat sink surface.
Sabelman, E. E.↗
Shock and vibration tests of a SNAP-8 NaK pump
The pump used for reactor cooling in the SNAP 8 space power system was subjected to the expected vehicle launch vibration, and shock loading in accordance with the SNAP 8 environmental specification. Subsequent disassembly revealed damage to the thrust bearing pins, which should be redesigned and strengthened. The unit was operational, however, when run in a test loop after reassembly.
Stromquist, A. J.↗
Aerodynamic static stability characteristics of the MSFC 33-foot pump fed booster at high angles of attack
Experimental aerodynamic investigations were conducted in the 14-inch trisonic wind tunnel during early February 1972 on a 0.00340 scale model of the 33-foot diameter space shuttle pump fed booster configuration. The basic configuration tested was a 40-deg cone/cylinder. Six component aerodynamic force and moment data were recorded over a Mach number range from 0.6 to 5.0, angles-of-attack from 50 to 90 deg at 0 deg sideslip and over a sideslip range from -10 to +10 deg at 60 and 80 deg angles-of-attack. Primary configuration variables were fin area and body cutout size.
Hamilton, T.↗