Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-oxygen Mixtures Assuming Frozen Composition
Title | Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-oxygen Mixtures Assuming Frozen Composition PDF eBook |
Author | Sanford Gordon |
Publisher | |
Pages | 70 |
Release | 1957 |
Genre | Charts, diagrams, etc |
ISBN |
Theoretical rocket performance for frozen composition during expansion was calculated for JP-4 fuel with several fluorine-oxygen mixtures for a large range of pressure ratios and oxidant-fuel ratios. The parameters included are 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. A correlation is given for the effect of chamber pressure on several of the parameters.
Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-oxygen Mixtures Assuming Equilibrium Composition
Title | Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-oxygen Mixtures Assuming Equilibrium Composition PDF eBook |
Author | Sanford Gordon |
Publisher | |
Pages | 78 |
Release | 1958 |
Genre | Aerodynamics |
ISBN |
Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-oxygen Mixtures Assuming Equilibrium Composition
Title | Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-oxygen Mixtures Assuming Equilibrium Composition PDF eBook |
Author | Sanford Gordon |
Publisher | |
Pages | 69 |
Release | 1958 |
Genre | Charts, diagrams, etc |
ISBN |
Theoretical rocket performance for equilibrium composition during expansion was calculated for JP-4 fuel with several fluorine-oxygen mixtures for a range of pressure ratios and oxidant-fuel ratios. The parameters included are specific impulse, combustion-chamber temperatures. Nozzle-exit temperature, molecular weight, characteristics velocity, coefficient of thrust, ratio of nozzle-exit area to throat area, specific heat at constant pressure, isentropic exponent, viscosity, thermal conductivity, and equilibrium gas compositions. A correlation is given for the effect of chamber pressure on several of the parameters.
Theoretical Performance of JP-4 Fuel with a 70-percent-fluorine - 30-percent Oxygen as a Rocket Propellant
Title | Theoretical Performance of JP-4 Fuel with a 70-percent-fluorine - 30-percent Oxygen as a Rocket Propellant PDF eBook |
Author | Sanford Gordon |
Publisher | |
Pages | 46 |
Release | 1956 |
Genre | Fluorine |
ISBN |
Theoretical Performance of JP-4 Fuel and Liquid Oxygen as a Rocket Propellant
Title | Theoretical Performance of JP-4 Fuel and Liquid Oxygen as a Rocket Propellant PDF eBook |
Author | Vearl N. Huff |
Publisher | |
Pages | 46 |
Release | 1956 |
Genre | Charts, diagrams, etc |
ISBN |
Theoretical rocket performance for frozen composition during expansion was calculated for the propellant combination JP-4 fuel and liquid oxygen at two chamber pressures and several pressure ratios and oxidant-fuel ratios.
Handling and Use of Fluorine and Fluorine-oxygen Mixtures in Rocket Systems
Title | Handling and Use of Fluorine and Fluorine-oxygen Mixtures in Rocket Systems PDF eBook |
Author | Harold W. Schmidt |
Publisher | |
Pages | 292 |
Release | 1967 |
Genre | Fluorine |
ISBN |
Theoretical Performance of JP-4 Fuel with a 70-percent-fluorine-30-percent-oxygen Mixture and a Rocket Propellant
Title | Theoretical Performance of JP-4 Fuel with a 70-percent-fluorine-30-percent-oxygen Mixture and a Rocket Propellant PDF eBook |
Author | Sanford Gordon |
Publisher | |
Pages | 38 |
Release | 1956 |
Genre | |
ISBN |