Effect of Thrust Per Element on Combustion Stability Characteristics of Hydrogen-oxygen Rocket Engines PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Effect of Thrust Per Element on Combustion Stability Characteristics of Hydrogen-oxygen Rocket Engines PDF full book. Access full book title Effect of Thrust Per Element on Combustion Stability Characteristics of Hydrogen-oxygen Rocket Engines by Reino J. Salmi. Download full books in PDF and EPUB format.
Author: Reino J. Salmi
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 36
Get Book Here
Book Description
Author: Reino J. Salmi
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 36
Get Book Here
Book Description
Author: Reino J. Salmi
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 27
Get Book Here
Book Description
Author: John P. Wanhainen
Publisher:
ISBN:
Category : Liquid propellant rocket engines
Languages : en
Pages : 52
Get Book Here
Book Description
Injector radial distribution and thrust chamber geometry effect on acoustic mode instability in hydrogen oxygen engines.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 92
Get Book Here
Book Description
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1504
Get Book Here
Book Description
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 478
Get Book Here
Book Description
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 470
Get Book Here
Book Description
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1716
Get Book Here
Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index
Author: Gilbert K. Sievers
Publisher:
ISBN:
Category : Hydrogen oxygen fuel cells
Languages : en
Pages : 88
Get Book Here
Book Description
Theoretical rocket performance data for the propellant combination of liquid hydrogen and liquid oxygen are presented in convenient graphical forms to permit rapid determination of specific impulse, vacuum specific impulse, and characteristic velocity. Data are presented for both frozen and equilibrium composition during expansion for chamber pressures of 15, 30, 60, 150, 300, 600, 900 and 1200 pounds per square inch absolute over a wide range of percent fuel from approximately 8 to 34 and area ratios to approximately 300. For rapid calculation of the theoretical nozzle performance with over- or under- expansion, separated flow, and introduction of propellants at different initial conditions or heat loss from the combustion chamber, the following theoretical data are also presented: combustion-chamber temperature, nozzle-exit temperature, and the ratio of chamber-pressure to nozzle-exit pressure. An easy method is given for estimating theoretical specific impulse at chamber pressures other than those presented.
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1320
Get Book Here
Book Description
