Two recently developed FORTRAN computer codes for high power Brayton and Rankine thermodynamic cycle analysis for space power applications are presented. The codes were written in support of an effort to develop a series of subsystem models for multimegawatt Nuclear Electric Propulsion, but their use is not limited just to nuclear heat sources or to electric propulsion. Code development background, a description of the codes, some sample input/output from one of the codes, and state future plans/implications for the use of these codes by NASA's Lewis Research Center are provided
Production of power in space for terrestrial use is of great interest in view of the rapidly rising ...
Space Rankine cycle power systems technology applied to ground-based power system
Nuclear thermal propulsion has long been considered an enabling technology for human missions to Mar...
The Nuclear Electric Propulsion (NEP) system optimization code consists of a master module and vario...
Comparison of Brayton and Rankine cycle magnetogasdynamic space power generation systems for use wit...
Analysis of reactor heated Brayton cycle space power plants - Models of gas and liquid-metal reactor...
Principles, characteristics, and technology development status of conversion systems for converting ...
Nuclear electric propulsion has been identified as an enabling technology for future NASA space scie...
Design, development, and performance of 35 to 150 kilowatt Brayton power conversion module and appli...
The feasibility of using Brayton power systems for nuclear electric spacecraft was investigated. The...
The objectives of the NASA Brayton Space Power Program and the advantages of achieving an isotope Br...
Development of combined turbine-magnetohydrodynamic generator operating in Brayton cycle with NERVA ...
The parametrically based closed Brayton cycle (CBC) computer design model was developed for inclusio...
Analysis of interplanetary cargo and piloted missions requires calculations of the performances and ...
Description and performance of electrical subsystem and components for Brayton power syste
Production of power in space for terrestrial use is of great interest in view of the rapidly rising ...
Space Rankine cycle power systems technology applied to ground-based power system
Nuclear thermal propulsion has long been considered an enabling technology for human missions to Mar...
The Nuclear Electric Propulsion (NEP) system optimization code consists of a master module and vario...
Comparison of Brayton and Rankine cycle magnetogasdynamic space power generation systems for use wit...
Analysis of reactor heated Brayton cycle space power plants - Models of gas and liquid-metal reactor...
Principles, characteristics, and technology development status of conversion systems for converting ...
Nuclear electric propulsion has been identified as an enabling technology for future NASA space scie...
Design, development, and performance of 35 to 150 kilowatt Brayton power conversion module and appli...
The feasibility of using Brayton power systems for nuclear electric spacecraft was investigated. The...
The objectives of the NASA Brayton Space Power Program and the advantages of achieving an isotope Br...
Development of combined turbine-magnetohydrodynamic generator operating in Brayton cycle with NERVA ...
The parametrically based closed Brayton cycle (CBC) computer design model was developed for inclusio...
Analysis of interplanetary cargo and piloted missions requires calculations of the performances and ...
Description and performance of electrical subsystem and components for Brayton power syste
Production of power in space for terrestrial use is of great interest in view of the rapidly rising ...
Space Rankine cycle power systems technology applied to ground-based power system
Nuclear thermal propulsion has long been considered an enabling technology for human missions to Mar...