The main problem for fluid mechanics analysis in the rocket engine is that of predicting the contained fuel mass for various propellant-to-fuel flow ratios. Tha analysis described here predicts a dimensionless measure of fuel mass called the fuel volume fraction. This analysis uses a coaxial free-jet computer code, and eddy viscosity equations developed for this code.
Estimates of fuel containment in a coaxial flow gas-core nuclear rocket
Nuclear Technology ; 12 , 2 ; 209-217
1971
9 Seiten, 10 Bilder, 7 Quellen
Aufsatz (Zeitschrift)
Englisch
ANTRIEB , BERECHNUNG , GAS , GESCHWINDIGKEIT , KERNBRENNSTOFF , KERNREAKTOR , RAKETE , RAUMFAHRT , REAKTORKERN
Magnetic fuel containment in the Gas Core Nuclear Rocket
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