The thermoradiative cell (TRC) is theoretically investigated, coupled with a radioisotope heat source, to provide primary power for a cubesat mission where photovoltaic power is impractical. Using a representative heat source, such as a single pellet of 238Pu from a General Purpose Heat Source (GPHS), provides 62.5 W of thermal energy. Using the 3K universe as a heat sink and a nominal power conversion efficiency of over 19%, a mass specific power of 30 W/kg is predicted. This represents a order-of-magnitude improvement over conventional radioisotope thermal generators. Realization of practical TRC devices by Metalorganic Vapor Phase Epitaxy (MOVPE), and development of identified low-bandgap materials such as InAs0.91Sb0.09 (0.28 eV) or InP0.63Sb0.37 (0.47 eV), is discussed.
Amit LalRajesh DuggiralaHui Li
Thomas E. HammelRussel BennettS. KeyserR.K. SieversWilliam D. Otting
Xin ZhangGuofeng YangMengqi YanL. K. AngYee Sin AngJincan Chen
Rajesh DuggiralaRonald G. PolcawichEugene ZakarMadan DubeyH. LiAmit Lal
Michael P. NielsenAndreas PuschPhoebe PearceMuhammad H. SazzadPeter J. ReeceMartin A. GreenNicholas J. Ekins‐Daukes