The design criteria and methodology of the Ariane 5 main stage are reviewed. The thrust chamber, main injector, and hydrogen pump are described. Differences between the cryogenic tanks of Ariane 5 and Ariane 4 are explained. The simulation and analysis programs are indicated.
Technology and Design Method Evolution of Cryogenic Propulsion Systems: Example of the Main Ariane 5 Stage
1988
10 pages
Report
Keine Angabe
Englisch
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