Thermodynamic Extrapolation of Rocket Performance Parameters
Thermionic spacecraft design study Phase 1 report, 4 Feb. 1969 - 4 Jan. 1970
Thermionic reactor ion propulsion spacecraft for unmanned outer planet exploration
Thermal Exposure of Ammunition on Board Ship. Part 4. Submarines
The radiant heat flux limit of bypass flow in a uranium plasma rocket
The open-cycle gas-core nuclear rocket engine: Some engineering considerations