Report presenting the theoretical rocket performance for frozen composition during expansion using JP-4 fuel and liquid oxygen at two chamber pressures and several pressure ratios and oxidant-fuel ratios. The parameters included specific impulse, combustion-chamber temperature, nozzle-exit temperature, molecular weight, characteristic velocity, coefficient of thrust, ratio of nozzle-exit area to throat area, specific heat at constant pressure, isentropic exponent, viscosity, and thermal conductivity.
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Report presenting the theoretical rocket performance for frozen composition during expansion using JP-4 fuel and liquid oxygen at two chamber pressures and several pressure ratios and oxidant-fuel ratios. The parameters included specific impulse, combustion-chamber temperature, nozzle-exit temperature, molecular weight, characteristic velocity, coefficient of thrust, ratio of nozzle-exit area to throat area, specific heat at constant pressure, isentropic exponent, viscosity, and thermal conductivity.
This report is part of the following collections of related materials.
National Advisory Committee for Aeronautics Collection
The National Advisory Committee for Aeronautics (NACA) was a U.S. federal agency founded on March 3, 1915 to undertake, promote, and institutionalize aeronautical research. On October 1, 1958 the agency was dissolved, and its assets and personnel transferred to the newly created National Aeronautics and Space Administration (NASA).
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Huff, Vearl N. & Fortini, Anthony.Theoretical performance of JP-4 fuel and liquid oxygen as a rocket propellant 1: frozen composition,
report,
April 17, 1956;
(https://digital.library.unt.edu/ark:/67531/metadc62469/:
accessed April 19, 2024),
University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu;
crediting UNT Libraries Government Documents Department.