Propulsion for space - The nuclear rocket.
Ground technology program for nuclear rocket development, discussing NERVA and KIWI programs
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Ground technology program for nuclear rocket development, discussing NERVA and KIWI programs
Pulse echo ultrasonic system automatically determines the temperature in the core of a nuclear rocket engine by measuring the transit time of an acoustic pulse in a wire sensor. The measurement is based on the fact that the speed of sound in the sensor material is a function of temperature.
Fast and moderated nuclear reactors, and feasibility of low-power lightweight reactors for nuclear rocket engine applications
Mathematical models of biological hazards from nuclear rocket engine flight failures
Postshutdown cooling requirements of tungsten water moderated nuclear rocket engines
High temperature ultrasonic temperature measurements in nuclear rocket engine to determine feasibility of rhenium sensor as high temperature sensor
Fabrication and test of flueric position servo for control drum of nuclear rocket engine
Fluid mechanics information applied to gaseous nuclear rocket engines
Open cycle gaseous fueled nuclear rocket engines, describing method of comparing engine characteristics with predicted engine performance
Economical feasibility of open and closed cycle vortex-stabilized gaseous nuclear rocket engines, investigating vortex flow characteristics
Gaseous reactor fluid mechanics for nuclear rocket engines, discussing experiments on geometries used in open cycle engine for acceptable uranium loss rate
Ultrasonic measurement of core material temperature in nuclear rocket engines
Flow characteristics of curved porous wall gas core reactors for nuclear rocket engines, visualizing simulated fuel flow with air-smoke combination
Gas-core nuclear rocket engine simulation by induction coupled plasma torch, determining gas flow patterns
Gas core nuclear rocket engine light and heavy species centrifugal separation by MHD-driven rotating flow, discussing fluid dynamic simulation results
Mathematical model avoiding repetitive tests costs for Nerva nuclear rocket engine
Solid core nuclear reactor engine variables, considering specific impulse, engine weight, operating life and engine thrust
NERVA nuclear rocket engine design technology program, discussing probabilistic techniques for reliability engineering