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Systematic Component Investigation of the Steady-State High-Temperature In-Pile Nuclear Thermal Propulsion Experimental Test Bed
Published in Nuclear Technology, 2022
Tyler R. Steiner, Richard H. Howard
A nuclear thermal rocket (NTR) produces thrust by heating, typically hydrogen propellant through a nuclear reactor core at roughly 2500 K (Ref. 1). This offers advantages over conventional chemical rockets by utilizing a less massive propellant and producing a larger specific impulse. A larger specific impulse presents the capability for faster transit times. Reducing travel time is essential to limit the deleterious effects of space radiation on the spacecraft’s crew and electronic systems. The nuclear thermal propulsion (NTP) environment consists of high-temperature hydrogen in a radiation field. Experimental testing is necessary to qualify components in such a harsh environment.