Analog computer and theoretical results are presented to show the nonlinear stability of any steady-state propellant temperature and flow in a typical nuclear rocket engine. This assurance of stability encourages design of schemes involving only propellant flow control or on-off drum controllers.
Stability of nuclear rocket engine dynamics
NUCLEAR APPL. ; 5 , 1 ; 35-45
1968
11 Seiten, 6 Bilder, 1 Tabelle, 17 Quellen
Article (Journal)
English
ANTRIEB , KERNREAKTOR , RAKETE , REGELUNG , STABILITAET
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