National Aeronautics and Space Administration, University of New Mexico. ... Alternator cooled by working fluid 1400-F turbine Inlet temperature Successfully completed 1100 h test program 27% efficiency demonstrated Brayton Isotope ... Figure 4 depicts the flow diagram and state points for the reference design points.
|Title||:||Proceedings of the Eighth Symposium on Space Nuclear Power Systems|
|Author||:||Mohamed S. El-Genk, Mark D. Hoover, United States. National Aeronautics and Space Administration, University of New Mexico. Institute for Space Nuclear Power Studies, Lewis Research Center, American Nuclear Society, American Institute of Physics|