Nuclear Thermal Propulsion - NASA
1500Nuclear Thermal Propulsion with Various Propellants - H2 1300 - NH3 1100 - H20 - CO2 900 700 500 300 100 . NTP mission proposals, from the moon ... Reported ternary-carbide fuel performance of operation at 3100 K for up to 1 hr. Carbide fuels also experience the most failure in the mid-band region where power densities are
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