The design of rocket engines is discussed, with particular reference to the Ariane launch vehicle. The parameters affecting engine efficiency are explained as well as the design problems. Trends are illustrated by the description of the HM60 engine which is a H2/O2 system in development for the future Ariane 5 launcher. The HM60 is designed for 900 kN thrust.
Grandeur et Servitudes de la Propulsion Par Moteurs Fusees a Liquides (Advantages and Limitations of Liquid Propellant Rocket Engines)
1984
8 pages
Report
No indication
English
ESPACE - Nouveaux moteurs fusées japonais
Online Contents | 2005
Moteurs, réacteurs, statoréacteurs, fusées
SLUB | 1959
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