Propellant Vaporization as a Design Criterion for Rocket-engine Combustion Chambers
Author : Richard J. Priem
Publisher :
Page : 64 pages
File Size : 19,85 MB
Release : 1960
Category : Combustion chambers
ISBN :
Author : Richard J. Priem
Publisher :
Page : 64 pages
File Size : 19,85 MB
Release : 1960
Category : Combustion chambers
ISBN :
Author : Marcus F. Heidmann
Publisher :
Page : 26 pages
File Size : 39,45 MB
Release : 1959
Category :
ISBN :
Author :
Publisher :
Page : 31 pages
File Size : 34,33 MB
Release : 1959
Category : Heat
ISBN :
Author : Richard J. Priem
Publisher :
Page : 68 pages
File Size : 30,36 MB
Release : 1960
Category : Combustion chambers
ISBN :
Author : Richard J. Priem
Publisher :
Page : 55 pages
File Size : 27,13 MB
Release : 1960
Category : Combustion chambers
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 1274 pages
File Size : 46,29 MB
Release : 1958
Category : Aeronautics
ISBN :
Author : Marcus F. Heidmann
Publisher :
Page : 19 pages
File Size : 35,16 MB
Release : 1958
Category : Rocket engines
ISBN :
An analysis is presented on the quantitative effect of incomplete propellant vaporization on rocket-engine performance. A relation between characteristic exhaust velocity c* and the percentages of oxidant and fuel vaporized and burned is given. The analysis shows that c* efficiencies of 70 to 90 percent can be realized when only half the fuel is vaporized, whereas c* efficiencies of about 60 percent can be realized when half the oxidant is vaporized. The specific relations between c* and propellant vaporized are presented graphically for the hydrogen-fluorine, hydrogen-oxygen, ammonia-fluorine, and JP-4 - oxygen propellant combinations. The analysis is applied to experimental data for these propellant combinations.
Author : Marcus F. Heidmann
Publisher :
Page : 22 pages
File Size : 49,84 MB
Release : 1959
Category : Rockets (Aeronautics)
ISBN :
Author :
Publisher :
Page : 462 pages
File Size : 36,38 MB
Release : 1967
Category :
ISBN :
Author :
Publisher :
Page : 68 pages
File Size : 30,44 MB
Release : 1960
Category : Aerodynamics
ISBN :