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General method and thermodynamic tables for computation of equilibrium composition and temperature of chemical reactions

General method for computation of equilibrium composition and temperature of chemical reactions

Tables of thermodynamic functions for analysis of aircraft-propulsion systems

Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen biflouride as oxidant for rocket engines 1: mixture of liquid ammonia and hydrazine

Analysis of rocket, ram-jet, and turbojet engines for supersonic propulsion of long-range missiles 1: rocket-engine performance

Analysis of Rocket, Ram-Jet, and Turbojet Engines for Supersonic Propulsion of Long-Range Missiles 2 - Rocket Missile Performance

Theoretical performance of JP-4 fuel with a 70-percent-fluorine - 30-percent oxygen as a rocket propellant.

Theoretical performance of JP-4 fuel and liquid oxygen as a rocket propellant 2: equilibrium composition

Theoretical performance of JP-4 fuel and liquid oxygen as a rocket propellant 1: frozen composition

Theoretical rocket performance of JP-4 fuel with mixtures of liquid ozone and fluorine


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