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Kerntechnik
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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
Multi-mission nuclear electric propulsion stage design.
Nuclear safety considerations for manned space flight
Unmanned spacecraft RTG shield optimization study Final report
Assessment of lightweight mobile nuclear power systems
Nuclear power for surface effect vehicle and aircraft propulsion
Investigation of mercury-flow ramp rates for startup of the SNAP-8 system
Experience with and improvements in containment vessel penetrations
Reactor power systems for manned earth orbital applications
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
Radiation flux mapping of OPE spacecraft models, phase 1
Isotope reentry vehicle design study - Conceptual design, phase 1A Topical report
Thermionic spacecraft design study Phase 1 report, 4 Feb. 1969 - 4 Jan. 1970
A split-core heat-pipe reactor for space power applications
The basic principles for optimum shielding of nuclear apparatus onboard spacecraft
Manned space flight nuclear system safety. Volume 6: Space base nuclear system safety plan
Mission performance potential of regeneratively cooled gas core nuclear rockets
The radiant heat flux limit of bypass flow in a uranium plasma rocket
Low thrust /high-impulse/ nuclear and electric space propulsion systems
Radiation physics research at Marshall Space Flight Center
AC ARC DYNAMICS, STABILIZATION AND STARTING CRITERIA.
Thermodynamic Extrapolation of Rocket Performance Parameters
STRAIN MEASUREMENTS ON A PRESSURIZED SOLID PROPELLANT GRAIN
An investigation of minimum drag atmospheric re-entry paths