Viewgraphs on the following are presented: (1) space nuclear thermal propulsion (SNTP) propellant management system; (2) SNTP cycle selection; (3) NTP system components unique design constraints; (4) bleed cycle unique design requirement for turbopump; (5) bleed cycle turbopump; (6) SNTP carbon-carbon turbine wheel; and (7) turbine development program.
Sntp Propellant Management System
1993
4 pages
Report
No indication
English
Space Technology , Electric & Ion Propulsion , Research Program Administration & Technology Transfer , Engine design , Management systems , Nuclear propulsion , Rocket propellants , Carbon-carbon composites , Design analysis , Temperature control , Turbine pumps , Turbine wheels , Nuclear rocket engines
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