Reactivity insertions in compact reactor cores due to fuel movement
Reactivity insertions in compact reactor cores due to fuel movement
Sullivan, R. E.↗
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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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Failure analysis of Delron inserts in the 60B20217-2 heat shield panel
Failure analysis of Delron inserts in 60B20217-2 heat shield panel
Teeter, L. W.↗
Improved throat inserts for ablative thrust chambers
Composite material development and structural design of improved throat inserts for ablative thrust chambers
Crump, D. N.↗
Neutronic effects on moderator insertion in fast-spectrum reactors
Neutronic effects of yttrium hydride moderator insertion in fast spectrum reactors
Mayo, W.↗
Tests of a single tube-in-shell water-boiling heat exchanger with a helical-wire insert and several inlet flow-stabilizing devices
Single tube-in-shell water-boiling heat exchanger performance with helical wire insert and flow stabilizing devices
Sekas, N. J.↗
Real-time targeting for the Apollo lunar orbit insertion maneuver.
Real time targeting for Apollo lunar orbit insertion maneuver burn, discussing impulsive maneuvers for flight control
Berry, R. L.↗
Insertion device for pressure testing
Test device which introduces either pressure or vacuum into a test pipe or tube, is insertable into the tested item where it secures itself into position and requires no external support. The unit has an operating range from zero to 25,000 psig and to any vacuum level that available equipment can reach.
Howland, B. T.↗
Development of the sterile insertion heat sealing tool and port opening Final report, 7 May 1968 - 31 Jan. 1969
Development of sterile insertion heat sealing tool and port opening
Source record↗
Frequency response of a forced flow single tube boiler with inserts and exit restriction
Frequency response of forced flow single tube boiler with inserts and exit restriction
Goodykoontz, J. H.↗
Evaluation of 7.8-inch-throat-diameter inserts and a unique cooling concept in a storable- propellant rocket engine
Nozzle insert evaluation and gas cooling concept in storable liquid propellant rocket engine
Peterson, D. A.↗
Thermochemical ablation of rocket nozzle insert materials Final report
Resistance of rocket nozzle throat insert materials to corrosion and melting
Clark, K. J.↗
Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor. Part 4 - Performance of bleed insert configuration no. 3
Evaluation of bleed insert configuration of single stage axial flow compressor
Koch, C. C.↗
Design, fabrication and evaluation of tungsten encapsulated silver infiltrated porous tungsten rocket nozzle inserts Final report
Rocket nozzle throat insert encapsulated in solid tungsten case
Price, J.↗
Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor. Part 5 - Performance of plain casing insert configuration with distorted inlet flow
Outer case bleeding or blowing effects on casing insert of single stage axial flow compressor with distorted inlet flow
Koch, C. C.↗
Development of Improved Throat Inserts for Ablative Rocket Engines
Throat and nozzle insert design for ablative rocket engine using storable propellants
Winter, Jerry M.↗
A radiometric method for measuring the insertion loss of radome materials.
Radome material insertion loss measurement by radiometric method noting error analysis
Seidel, B. L.↗
Precision insertion-loss calibrations at 90 GHz.
Dual channel waveguide insertion loss test set for calibrations at 90 GHz in radio astronomy and communication systems, using sprayed thermistor mount
Oltmans, D. A.↗
Real-time targeting for the Apollo lunar orbit insertion maneuver.
Real time targeting for Apollo lunar orbit insertion maneuver burn, discussing impulsive maneuvers for flight control
Berry, R. L.↗