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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 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 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 70-30 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 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.

Handling and Use of Fluorine and Fluorine-oxygen Mixtures in Rocket Systems

Handling and Use of Fluorine and Fluorine-oxygen Mixtures in Rocket Systems PDF Author: Harold W. Schmidt
Publisher:
ISBN:
Category : Fluorine
Languages : en
Pages : 292

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


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


The Chemistry of Propellants

The Chemistry of Propellants PDF Author: S. S. Penner
Publisher: Elsevier
ISBN: 1483221296
Category : Technology & Engineering
Languages : en
Pages : 666

Book Description
The Chemistry of Propellants is a collection of papers and comments presented at the meeting on “The Chemistry of Propellants , held in Paris, France on June 8-12, 1959, organized by the AGARD Combustion and Propulsion Panel. This book is organized into six parts encompassing 25 chapters that serve as an introduction to the broad and important subject of propellant chemistry and propulsion applications. The first part deals with the sources, availability, and comparative costing of propulsion system. The second and third parts discuss the theoretical, thermodynamic, and experimental aspects of liquid and solid propellants. The fourth part examines the main problems concerning preparation, storage, and use of propellants for ramjet, while the fifth part looks into the factors leading to deposits in jet engines and some of the consequences of their existence. The sixth part covers the advantages of the high energy chemical propellants, including fluorine and hydrogen. Combustion and propulsion scientists and researchers will find this book beneficial.

Handling and Use of Fluorine and Fluorine- Oxygen Mixtures in Rocket Systems

Handling and Use of Fluorine and Fluorine- Oxygen Mixtures in Rocket Systems PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 292

Book Description


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