Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 180
Book Description
Pressurization Systems for Liquid Rockets
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 180
Book Description
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 180
Book Description
Pressurization System for Liquid Rockets
Author: National Aeronautics and Space Administration
Publisher: CreateSpace
ISBN: 9781499162103
Category :
Languages : en
Pages : 176
Book Description
The purpose of this monograph is to organize and present, for effective use in deign, the significance experience and knowledge accumulated in development and operational programs to date. It reviews and assesses current design practices, and from them establishes firm guidance for achieving consistency in design, increased reliability in the end product, and greater efficiency in the design effort.
Publisher: CreateSpace
ISBN: 9781499162103
Category :
Languages : en
Pages : 176
Book Description
The purpose of this monograph is to organize and present, for effective use in deign, the significance experience and knowledge accumulated in development and operational programs to date. It reviews and assesses current design practices, and from them establishes firm guidance for achieving consistency in design, increased reliability in the end product, and greater efficiency in the design effort.
Advanced Pressurization System for Liquid Rockets
Author: R. A. Byron
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 7
Book Description
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 7
Book Description
Chemical Kinetics in Combustion and Reactive Flows: Modeling Tools and Applications
Author: V. I. Naoumov
Publisher: Cambridge University Press
ISBN: 1108427049
Category : Science
Languages : en
Pages : 449
Book Description
Introduces advanced mathematical tools for the modeling, simulation, and analysis of chemical non-equilibrium phenomena in combustion and flows, following a detailed explanation of the basics of thermodynamics and chemical kinetics of reactive mixtures. Researchers, practitioners, lecturers, and graduate students will find this work valuable.
Publisher: Cambridge University Press
ISBN: 1108427049
Category : Science
Languages : en
Pages : 449
Book Description
Introduces advanced mathematical tools for the modeling, simulation, and analysis of chemical non-equilibrium phenomena in combustion and flows, following a detailed explanation of the basics of thermodynamics and chemical kinetics of reactive mixtures. Researchers, practitioners, lecturers, and graduate students will find this work valuable.
Rocket Propellant and Pressurization Systems
Author: Elliot Ring
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 330
Book Description
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 330
Book Description
Pressurization System Analysis for Cryogenic Propulsion Systems
Author: Frederick Chopp
Publisher:
ISBN:
Category :
Languages : en
Pages : 33
Book Description
Stored gas pressurization and boost pump liquid rocket engine propellant transfer systems were investigated to compare their suitability for use on hydrogen-oxygen upper stage vehicles. The purpose of this document is to present the results of this study and to describe the method of analysis used. System comparisons were based on the overall system weight. The mission duty cycle, NPSH, propellant weight, and propellant type were held constant. Results indicated that liquid transfer with boost pumps will provide a minimum system weight for the selected baseline configuration and ground rules. For stored gas pressurization, it was determined that storage of the gas bottle should be in the hydrogen tank with the pressurant heated prior to entering the tanks. Optimum pressurant temperature for the hydrogen tank was found to be 350 R. No calculations were made to optimize the oxygen tank pressurant temperature. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 33
Book Description
Stored gas pressurization and boost pump liquid rocket engine propellant transfer systems were investigated to compare their suitability for use on hydrogen-oxygen upper stage vehicles. The purpose of this document is to present the results of this study and to describe the method of analysis used. System comparisons were based on the overall system weight. The mission duty cycle, NPSH, propellant weight, and propellant type were held constant. Results indicated that liquid transfer with boost pumps will provide a minimum system weight for the selected baseline configuration and ground rules. For stored gas pressurization, it was determined that storage of the gas bottle should be in the hydrogen tank with the pressurant heated prior to entering the tanks. Optimum pressurant temperature for the hydrogen tank was found to be 350 R. No calculations were made to optimize the oxygen tank pressurant temperature. (Author).
Fundamentals of Theory and Calculation of Liquid-propellant Rocket Engines, Volume i
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 300
Book Description
Theoretical and design principles of liquid rocket engines are presented. Extensive coverage is given to processes taking place in the combustion chamber, calculations of mixing systems, the cooling and contour calculation of the nozzles, calculation and selection of optimal parameters, turbopump and fuel feed pressurization systems, generation of the working medium for the turbine and fuel feed pressurization system, design and integration of pneumohydraulic systems for liquid rocket engines, calculation methods and selection of a liquid rocket engine parameters with a closed generation circuit of the working medium for the turbine. Basic theoretical and design principles of processes taking place in different types of liquid rocket engines are presented. The operation of main subsystems and the calculation of their characteristics are discussed. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 300
Book Description
Theoretical and design principles of liquid rocket engines are presented. Extensive coverage is given to processes taking place in the combustion chamber, calculations of mixing systems, the cooling and contour calculation of the nozzles, calculation and selection of optimal parameters, turbopump and fuel feed pressurization systems, generation of the working medium for the turbine and fuel feed pressurization system, design and integration of pneumohydraulic systems for liquid rocket engines, calculation methods and selection of a liquid rocket engine parameters with a closed generation circuit of the working medium for the turbine. Basic theoretical and design principles of processes taking place in different types of liquid rocket engines are presented. The operation of main subsystems and the calculation of their characteristics are discussed. (Author).
Liquid Rocket Booster (Lrb) for the Space Transportion System (Sts) Systems Study. Appendix D
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722617202
Category :
Languages : en
Pages : 60
Book Description
Trade studies plans for a number of elements in the Liquid Rocket Booster (LRB) component of the Space Transportation System (STS) are given in viewgraph form. Some of the elements covered include: avionics/flight control; avionics architecture; thrust vector control studies; engine control electronics; liquid rocket propellants; propellant pressurization systems; recoverable spacecraft; cryogenic tanks; and spacecraft construction materials. Unspecified Center...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722617202
Category :
Languages : en
Pages : 60
Book Description
Trade studies plans for a number of elements in the Liquid Rocket Booster (LRB) component of the Space Transportation System (STS) are given in viewgraph form. Some of the elements covered include: avionics/flight control; avionics architecture; thrust vector control studies; engine control electronics; liquid rocket propellants; propellant pressurization systems; recoverable spacecraft; cryogenic tanks; and spacecraft construction materials. Unspecified Center...
Pressurization Systems Design Guide: System analysis and selection
Author: Aerojet-General Corporation
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 516
Book Description
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 516
Book Description
Pressurization Systems Design Guide: pt.A-B. Design procedures and data
Author: Aerojet-General Corporation
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 458
Book Description
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 458
Book Description