The principal components, i.e., the combustion chamber and the nozzle, of the thrust chamber of a rocket engine are presented and discussed together with their performance parameters. Injectors, engine cycles, and igniters are discussed. Methods are given for their quantitative design. Cooling systems and combustion stabilising devices are also presented.
The Thrust Chamber Assembly
Springer Aerospace Techn.
27.09.2020
140 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Thrust Chamber Assembly Photographs
NTIS | 1966
NTIS | 1965
|Throttling thrust-chamber control
Engineering Index Backfile | 1951
|