Publication Date:
2013-08-31
Description:
The Nuclear Electric Propulsion (NEP) system optimization code consists of a master module and various submodules. Each of the submodules represents a subsystem within the total NEP power system. The master module sends commands and input data to each of the submodules and receives output data back. Rocketdyne was responsible for preparing submodules for the power conversion (both K-Rankine and Brayton), heat rejection, and power management and distribution.
Keywords:
SPACECRAFT PROPULSION AND POWER
Type:
NASA. Lewis Research Center, Nuclear Propulsion Technical Interchange Meeting, Volume 2; p 821-838
Format:
application/pdf