Nuclear rocket simulator tests, flow initiation with no turbine gas tank pressure, 35 PSIA Run 1
Nuclear reactor simulator test - liquid hydrogen run, instrumentation and data acquisition system operational procedure checkout
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Nuclear reactor simulator test - liquid hydrogen run, instrumentation and data acquisition system operational procedure checkout
Liquid hydrogen nuclear reactor simulator tests - determination of flow iniation with turbine accelerated tank pressure 50 psia
Control analysis of NERVA engine at power range operating conditions
Almost all of the fluid mechanics research associated with the coaxial flow gas core reactor ended abruptly with the interruption of NASA's space nuclear program because of policy and budgetary considerations in 1973. An overview of program accomplishments is presented through a review of the experiments conducted and the analyses performed. Areas are indicated where additional research is required for a fuller understanding of cavity flow and of the factors which influence cold and hot flow containment. A bibliography is included with graphic material.
TAPAT computer program for design and analysis of radiation shields in nuclear rocketry
The experimental and theoretical investigations conducted during the period from September 1969 through September 1972 are reported which were directed toward obtaining information necessary to determine the feasibility of the full-scale nuclear light bulb engine, and of small-scale nuclear tests involving fissioning uranium plasmas in a unit cell installed in a driver reactor, such as the Nuclear Furnace. Emphasis was placed on development of RF simulations of conditions expected in nuclear tests in the Nuclear Furnace. The work included investigations of the following: (1) the fluid mechanics and containment characteristics of one-component and two-component vortex flows, both unheated and RF-induction heated; (2) heating of particle-seeded streams by thermal radiation from a dc arc to simulate propellant heating; (3) condensation and separation phenomena for metal-vapor/heated-gas mixtures to provide information for conceptual designs of components of fuel exhaust and recycle systems; (4) the characteristics of the radiant energy spectrum emitted from the fuel region, with emphasis on definition of fuel and buffer-gas region seed systems to reduce the ultraviolet radiation emitted from the nuclear fuel; and (5) the effects of nuclear radiation on the optical transmission characteristics of transparent materials.
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Revision of rover program, rift project, and nerva & kiwi reactors
Liapunov method for closed loop time optimal control of linear systems with bounded control norm using eigenvector scalar product solution for Hamilton-Jacobi equation
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Second Method of Liapunov, Popov frequency criterion, and matrix inequality method used to study stability of nonlinear and/or time dependent control systems
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Predicting flow patterns of vortex tubes at high Reynolds numbers
NERVA materials program extending data to account for synergistic influence of cryogenic and radiation environment
Heat transfer coefficients in rocket nozzle cooling passages predicted by equation developed from hydrogen flow experiments
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Instrumentation design problems connected with NERVA, considering high gamma and neutron radiations and temperature environments