NASA NTRS · 19920001894
Propulsion system needs
Abstract
The needs of the designer of a solid core nuclear rocket engine are discussed. Some of the topics covered include: (1) a flight thrust module/feed system module assembly; (2) a nuclear thermal rocket (NTR), expander cycle, dual T/P; (3) turbopump operating conditions; (4) typical system parameters; (5) growth capability composite fuel elements; (6) a NTR radiation cooled nozzle extension; (7) a NFS-3B Feed System; and (8) a NTR Integrated Pneumatic-Fluidics Control System.
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Gunn, Stanley. 1991-01-01. Propulsion system needs. https://ntrs.nasa.gov/citations/19920001894
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