Author: Sanford GordonPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 78
Book Description
Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-oxygen Mixtures Assuming Equilibrium Composition
Author: Sanford GordonPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 78
Book Description
Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-oxygen Mixtures Assuming Equilibrium Composition
Author: Sanford GordonPublisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 69
Book Description
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 Rocket Performance of JP-4 Fuel with Several Fluorine-oxygen Mixtures Assuming Frozen Composition
Author: Sanford GordonPublisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 70
Book Description
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 Performance of JP-4 Fuel with a 70-30 Mixture of Fluorine and Oxygen as a Rocket Propellant
Author: Sanford GordonTheoretical Rocket Performance of JP-4 Fuel with Mixtures of Liquid Ozone and Fluorine
Author: Vearl N. HuffPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 22
Book Description
Theoretical Performance of JP-4 Fuel with a 70-percent-fluorine - 30-percent Oxygen as a Rocket Propellant
Author: Sanford GordonPublisher:
ISBN:
Category : Fluorine
Languages : en
Pages : 46
Book Description
Theoretical Performance of JP-4 Fuel and Liquid Oxygen as a Rocket Propellant
Author: Vearl N. HuffPublisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 58
Book Description
Data were calculated for equivalence ratios of 1 to 3, chamber pressures of 300 and 600 pounds per square inch absolute, and pressure ratios of 1 to 1500. Parameters included are specific impulse, combustion and 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 which permits determination of performance for a wide range of chamber pressure.
Handling and Use of Fluorine and Fluorine-oxygen Mixtures in Rocket Systems
Author: Harold W. SchmidtPublisher:
ISBN:
Category : Fluorine
Languages : en
Pages : 292
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
Author: