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    Preliminary analysis of three cycles for nuclear propulsion of aircraft (1950)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: A preliminary study was made of the feasibility of three cycles for nuclear propulsion of aircraft: a direct-air-turbojet, a binary liquid-metal turbojet, and a helium compressor jet. All three cycles appeared feasible for flight at a Mach number of 0.9 and altitudes up to 50,000 feet; the liquid-metal cycle appeared feasible for flight at a Mach number of 1.5. The air and helium cycles resulted in heavier aircraft than did the liquid-metal cycle, particularly at a Mach number of 1.5. The relative advantage of the liquid-metal cycle became greater as the flight speed and altitude increased, and as the reactor wall temperature decreased.
    Keywords: Propellants and Fuels
    Type: NACA-RM-E50H24
    Format: application/pdf
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