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Online Books by

Sanford Gordon

Books from the extended shelves:

• Gordon, Sanford: An analytical investigation of three general methods of calculating chemical-equilibrium compositions (National Aeronautics and Space Administration, 1960), also by Frank J. Zeleznik and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Gordon, Sanford: Computer program for calculation of complex chemical equilibrium compositions, rocket performance, incident and reflected shocks, and Chapman-Jouguet detonations (Scientific and Technical Information Office, National Aeronautics and Space Administration, 1980), also by Bonnie J. McBride, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Gordon, Sanford: Fortran IV program for calculation of thermodynamic data (National Aeronautics and Space Administration :, 1967), also by Bonnie J. McBride and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Gordon, Sanford: A General IBM 704 or 7090 Computer Program for computation of chemical equilibrium compositions, rocket performance, and Chapman-Jouguet dentonations / Frank J. Zeleznik and Sanford Gordon. (National Aeronautics and Space Administration :, 1962), also by Frank J. Zeleznik and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Gordon, Sanford: A general method for automatic computation of equilibrium compositions and theoretical rocket performance of propellants (National Aeronautics and Space Administration, 1959), also by Vearl N. Huff, Frank J. Zeleznik, and Lewis Research Center (page images at HathiTrust)
• Gordon, Sanford: NASA TN D-1737 (National Aeronautics and Space Administration, 1963), also by Frank J. Zeleznik, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Gordon, Sanford: Simulations least-squares approximation of a function and its first integrals with application to thermodynamic data. (National Aeronautics and Space Administration :, 1961), also by Frank J. Zeleznik and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Gordon, Sanford: Theoretical performance of JP-4 fuel and liquid oxygen as a rocket propellant : II. Equilibrium composition (National Advisory Committee for Aeronautics, 1956), also by Vearl N. Huff, Anthony Fortini, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Gordon, Sanford: Theoretical performance of JP-4 fuel with a 70-percent-fluorine - 30-percent oxygen as a rocket propellant. [Part] I, Frozen composition (National Advisory Committee for Aeronautics, 1956), also by Vearl N. Huff, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Gordon, Sanford: Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen bifluoride as oxidant for rocket engines. [Part] 3, Liquid ammonia (National Advisory Committee for Aeronautics, 1952), also by Vearl N. Huff and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Gordon, Sanford: Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen bifluoride as oxidant for rocket engines. [Part] 2, Hydrazine (National Advisory Committee for Aeronautics, 1952), also by Vearl N. Huff and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Gordon, Sanford: Theoretical performance of liquid ammonia with liquid oxygen as a rocket propellant (National Advisory Committee for Aeronautics, 1958), also by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Gordon, Sanford: Theoretical rocket performance of JP-4 fuel with mixtures of liquid ozone and fluorine (National Advisory Committee for Aeronautics, 1956), also by Vearl N. Huff and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Gordon, Sanford: Theoretical rocket performance of JP-4 fuel with several fluorine-oxygen mixtures assuming equilibrium composition (National Advisory Committee for Aeronautics, 1958), also by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Gordon, Sanford: Theoretical rocket performance of JP-4 fuel with several fluorine-oxygen mixtures assuming frozen composition (National Advisory Committee for Aeronautics, 1957), also by Kenneth S. Drellishak, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Gordon, Sanford: Thermodynamic and transport combustion properties of hydrocarbons with air : compositions corresponding to kelvin temperatures schedules in part I (National Aerodynamics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)

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