A basic requirement of the test facility is to apply as far as possible flight conditions to the tested rocket engine [10]. It is mandatory that all interfaces between the bench and the engine are adjusted to the same values as on the launcher. Furthermore the evolution of interface parameters versus the time is regulated according the evolution during flight.
Simulation of Flight Conditions
Springer Aerospace Techn.
2010-08-20
10 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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