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- W18786588 abstract "A procedure was developed to calculate the critical fuel mass, including the effects of propellant pressure, for coaxial-flow gas-core reactors operating at 196,600 newtons thrust and 4400 seconds specific impulse. Data were generated for a range of cavity diameter, reflector-moderator thickness, and quantity of structural material. Also presented are such core characteristics as upper limits on cavity pressure, spectral hardening in very-high-temperature hydrogen, and reactivity coefficients." @default.
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- W18786588 date "1972-04-01" @default.
- W18786588 modified "2023-09-27" @default.
- W18786588 title "Neutronics analysis of an open-cycle high-impulse gas core reactor concept" @default.
- W18786588 hasPublicationYear "1972" @default.
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