Author: Sanford Gordon
Publisher:
ISBN:
Category : Fluorine
Languages : en
Pages : 46
Book Description
Theoretical Performance of JP-4 Fuel with a 70-percent-fluorine - 30-percent Oxygen as a Rocket Propellant
Author: Sanford Gordon
Publisher:
ISBN:
Category : Fluorine
Languages : en
Pages : 46
Book Description
Publisher:
ISBN:
Category : Fluorine
Languages : en
Pages : 46
Book Description
Theoretical Performance of JP-4 Fuel with a 70-percent-fluorine-30-percent-oxygen Mixture and a Rocket Propellant
Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-oxygen Mixtures Assuming Frozen Composition
Author: Sanford Gordon
Publisher:
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.
Publisher:
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
Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-oxygen Mixtures Assuming Equilibrium Composition
Author: Sanford Gordon
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 78
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 78
Book Description
Theoretical Performance of JP-4 Fuel and Liquid Oxygen as a Rocket Propellant
Author: Vearl N. Huff
Publisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 46
Book Description
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.
Publisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 46
Book Description
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.
Theoretical Rocket Performance of JP-4 Fuel with Mixtures of Liquid Ozone and Fluorine
Author: Vearl N. Huff
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 22
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 22
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Research Abstracts and Reclassification Notice
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 716
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 716
Book Description