Feasibility tests of a radioisotope-type ablation-measuring system.
Feasibility of making continuous measurements of ablation of spacecraft heat shield by use of radioisotopes embedded in heat shield
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Feasibility of making continuous measurements of ablation of spacecraft heat shield by use of radioisotopes embedded in heat shield
Voltage transformation and power/energy utilization of radioisotopic thermoelectric generator source /RTG/ for space applications, analyzing components, inverter/converter circuits, etc
Radioisotope heating for ionizer temperature of contact ionization thrustors for satellite attitude control and stationkeeping, studying power source mass saving
A method and computer program were developed for calculating the creep and optimizing the dimensions of capsules filled with alpha-emitting radioisotopes. The method solves an integral equation that was developed assuming linear accumulation of partial creep lives and relating life to time-dependent stress and temperature using the Larson-Miller parameter. The computer program, CAPSUL, is written in Fortran language for the IBM 360/75 computer. The program makes a least squares fit of the creep life function using conventional constant stress, constant temperature creep data. Dimensions of capsules having maximum thermal power per unit of weight, volume, or area are calculated for a given creep life and pressure-temperature history using a numerical Lagrange Multiplier formulation. The program also calculates the life to a prescribed strain for capsules of given dimensions and pressure-temperature history. The method has been used to analyze creep data for the alloys 304 stainless steel, Hastelloy N, Cb-1% Zr, FS-85, and T-222.
Parametric analysis of radioisotope cascaded thermoelectric generators with Si-Ge first stage and PbTe second stage
A parametric analysis of a radioisotope-thermoelectric power generator is presented. A cylindrical heat-source geometry was assumed with either lead telluride or silicon-germanium thermoelectric elements located around the lateral surface of the fuel block. Generator performance, rather than overall power-system performance, was analyzed; that is, such mission dependent considerations as nuclear shielding, reentry protection, and power conditioning were not included.
Solar and radioisotope Brayton cycle power supplies
Flow type detector for beta emitting radioisotopes produces linear response and rapid radioactivity washout
Solar or radioisotope Brayton power system efficiencies estimated for ground test configurations
Radioisotope thermoelectric generator concepts for Voyager Surface Lander, noting PbTe and GeSi thermoelectrics, reentry body shapes and integration considerations
Radioisotope electrogenerators based on beta emitting fuels, discussing design and aerospace applications
Radioisotopic color scanning of pulmonary aeroemboli in decompression sickness, noting dog experiment results and role of dextran infusion in recovery
Electrically heated and radioisotope heated thrusters for satellite attitude control and stationkeeping
Design and safety of radioisotope heater
Research and development of radioisotope heating equipment for manned spacecraft temperature control
Histopathological evidence for pulmonary emboli in experimental decompression sickness diagnosed by radioisotopic lung scanning
Radioisotopes and subliming materials for spacecraft orientation and microthrustor design optimization
Compatibility and shielding analysis of science instruments in spacecraft containing radioisotope thermoelectric generator