2017 IEEE Aerospace Conference 2017
DOI: 10.1109/aero.2017.7943892
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Dynamic Radioisotope Power System development for space exploration

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Cited by 6 publications
(2 citation statements)
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“…The baseline mission can use currently available MMRTGs (Lee & Bairstow 2015). However, the ability to use either the next-generation RTG (Matthes et al 2018) or the dynamic RPS (Qualls et al 2017) systems currently under development by NASA with estimated launch availability dates of 2026 and 2030, respectivelywhich were baselined for the recent Neptune Odyssey mission concept (Rymer et al 2021)-would provide 20%-380% greater end-of-life power than the MMRTGs and significantly enhance the capability of a New Frontiers-class Uranus orbiter.…”
Section: Required Mission Design Scope and Considerationsmentioning
confidence: 99%
“…The baseline mission can use currently available MMRTGs (Lee & Bairstow 2015). However, the ability to use either the next-generation RTG (Matthes et al 2018) or the dynamic RPS (Qualls et al 2017) systems currently under development by NASA with estimated launch availability dates of 2026 and 2030, respectivelywhich were baselined for the recent Neptune Odyssey mission concept (Rymer et al 2021)-would provide 20%-380% greater end-of-life power than the MMRTGs and significantly enhance the capability of a New Frontiers-class Uranus orbiter.…”
Section: Required Mission Design Scope and Considerationsmentioning
confidence: 99%
“…To develop these convertors, the RPS Program, working with the DOE, is conducting two major efforts: one that matures the dynamic technology of the convertors, called Dynamic Convertor Technology (DCT), managed under the Program's Stirling Convertor Technology Project; and, another that grounds the technology maturation from a mission and system perspective, called Dynamic RPS (DRPS) engineering, managed under the Program's Systems Formulation and Mission Integration function. 6 Key activities of this work includes 1) a procurement activity intended to result in a design and breadboard level of hardware, 2) the establishment of a Surrogate Mission Team (SMT) to develop generator system and interface requirements, and perform engineering system trades, 3) engagement with industry to assess technologies to understand the technology readiness and risks to consider for a near-term flight development activity, and 4) an activity that evaluates the use of the convertors within RPS concepts. NASA and DOE are examining these general concepts; however, a specific dynamic generator is not being designed.…”
Section: Dynamic Rps Statusmentioning
confidence: 99%