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Kerntechnik
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Small nuclear light bulb engines with cold beryllium reflectors.
The open-cycle gas-core nuclear rocket engine: Some engineering considerations
Experimental evaluation of tantalum/stainless steel mercury boilers for the SNAP 8 program
Safety determinations in nuclear power licensing /a critical view/.
Effects of proton irradiation on several spacecraft science components.
Proceedings of the National Symposium on Natural and Manmade Radiation in Space
The effects of radiation on science instruments during Grand Tour type missions
Effects of sublimation on silicon-germanium RTG performance
Unique production problems encountered in development of NERVA space engine
A study of heat pipe applications in nuclear aircraft propulsion systems Final report
An aerospace nuclear safety analysis of a Pm sub 2 O sub 3 radioisojet thruster.
Experimental exploration of recirculation zone in the gas-core nuclear rocket concept.
NERVA program Summary report no. 6, period ending 30 Sep. 1967
AEC-NASA Space Nuclear Propulsion Office instrumentation evaluation NRX-A2 tests
SUCCESSIVE APPROXIMATION TECHNIQUES FOR TRAJECTORY OPTIMIZATION
Propulsion system requirements for a multi-mission nuclear electric spacecraft.
Post-shutdown temperature of a buried reactor system for a lunar based power plant
Electric propulsion mission analysis - Terminology and nomenclature
Cold-flow startup test summary of a full-scale nuclear rocket engine using a radial turbopump
Open-cycle and light-bulb types of vortex- stabilized gaseous nuclear rockets.
Nuclear electric propulsion stage requirements and description
Performance potential of gas-core and fusion rockets: A mission applications survey
Experimental investigations of SNAP-8 shutdown characteristics
Investigation of gaseous nuclear rocket technology Quarterly progress report, 16 Sep. - 15 Dec. 1967
A reactor concept for space power employing thermionic diodes and pipes
Performance potential of gas-core and fusion rockets - A mission applications survey.
Nuclear power for surface effect vehicle and aircraft propulsion
Evaluation of critical mass for open-cycle, gas-core rocket reactors
Mechanical evaluation of TAA 5/4 after 10,823 hours of operation in PCS-1
Isotope reentry vehicle design study - Conceptual design, phase 1A Topical report