Theoretical Performance of JP-4 Fuel with a 70-percent-fluorine - 30-percent Oxygen as a Rocket Propellant PDF Download

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Theoretical Performance of JP-4 Fuel with a 70-percent-fluorine - 30-percent Oxygen as a Rocket Propellant

Theoretical Performance of JP-4 Fuel with a 70-percent-fluorine - 30-percent Oxygen as a Rocket Propellant PDF 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

Theoretical Performance of JP-4 Fuel with a 70-percent-fluorine - 30-percent Oxygen as a Rocket Propellant PDF 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 Mixture and a Rocket Propellant

Theoretical Performance of JP-4 Fuel with a 70-percent-fluorine-30-percent-oxygen Mixture and a Rocket Propellant PDF Author: Sanford Gordon
Publisher:
ISBN:
Category :
Languages : en
Pages : 38

Book Description


Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-oxygen Mixtures Assuming Frozen Composition

Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-oxygen Mixtures Assuming Frozen Composition PDF 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.

Theoretical Performance of JP-4 Fuel with a 70-30 Mixture of Fluorine and Oxygen as a Rocket Propellant

Theoretical Performance of JP-4 Fuel with a 70-30 Mixture of Fluorine and Oxygen as a Rocket Propellant PDF Author: Sanford Gordon
Publisher:
ISBN:
Category :
Languages : en
Pages : 49

Book Description


Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-oxygen Mixtures Assuming Equilibrium Composition

Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-oxygen Mixtures Assuming Equilibrium Composition PDF Author: Sanford Gordon
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 78

Book Description


Theoretical Performance of JP-4 Fuel and Liquid Oxygen as a Rocket Propellant

Theoretical Performance of JP-4 Fuel and Liquid Oxygen as a Rocket Propellant PDF 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.

Theoretical Rocket Performance of JP-4 Fuel with Mixtures of Liquid Ozone and Fluorine

Theoretical Rocket Performance of JP-4 Fuel with Mixtures of Liquid Ozone and Fluorine PDF Author: Vearl N. Huff
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 22

Book Description


Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388

Book Description


A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388

Book Description


Research Abstracts and Reclassification Notice

Research Abstracts and Reclassification Notice PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 716

Book Description