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- Charts for the Computation of Equilibrium Composition of Chemical Reactions in the Carbon-Hydrogen-Nitrogen System at Temperatures from 2000 to 5000 Degrees K
- Charts for the Computation of Equilibrium Composition of Chemical Reactions in the Carbon-Hydrogen-Oxygen-Nitrogen System at Temperatures From 2000 to 5000 K
- General method for computation of equilibrium composition and temperature of chemical reactions
- Tables of thermodynamic functions for analysis of aircraft-propulsion systems
- General method and thermodynamic tables for computation of equilibrium composition and temperature of chemical reactions
- 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 2 - Rocket Missile Performance
- Analysis of rocket, ram-jet, and turbojet engines for supersonic propulsion of long-range missiles 1: rocket-engine 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