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Dynamic Radioisotope Power System (DRPS) Design Reference Mission (DRM) Lunar RoverThe Radioisotope Power Systems (RPS) Program tasked the Compass Team to evaluate use of Dynamic Radioisotope Power Systems (DRPS) for lunar science rovers. The object was to identify their advantages and challenges as well as to influence the technology developments with flight-type requirements. This was easily done by using the promising Volatiles Investigating Polar Exploration Rover (VIPER) solar- powered rover mission as a platform to ‘swap in’ a DRPS. The ‘pickup truck bed’ approach allowed both simplified installation and operation of the DRPS while keeping the forward lunar surface ‘blocked’ from the DRPS waste heat which could sublimate the icy surface. It was found that with the Stirling DRPS option the mass is within the planned VIPER lander capability and is very close to VIPER mass and size (the DRPS replaces large battery pack/solar arrays). The Stirling DRPS option produced ~300 Watts electrical (We) using six general purpose heat source (GPHS) bricks and eight Stirling convertors. Replacing the solar/battery power with radioisotope power allows a continuous presence (instead of 6 hours) in a permanently shadowed region (PSR) and over 18 months of operations with minimal science impact (rearward surface heating). It was also found that use of a dynamic system (instead of a thermoelectric system) reduces the heat impact on the science environment two-to-three times. The DRPS, along with a relay link (like Gateway), can provide continuous access to PSRs. The system was also found to be capable of roving for 8 hours per day with a range of over 500 km in 18 months. Preliminary cost estimates fit into a Class D mission but only assuming VIPER heritage and launch, lander, operations, nuclear specific costs [National Environmental Policy Act (NEPA), fueling, transport, Launch Services Program (LSP), etc.] and DRPS are not included.
Document ID
20220013310
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Steven Oleson
(Glenn Research Center Cleveland, Ohio, United States)
Elizabeth Turnbull
(Glenn Research Center Cleveland, Ohio, United States)
Paul Schmitz
(Power Computing Solutions Inc. Avon Lake, Ohio, USA)
Kirby Runyon
(Johns Hopkins University Applied Physics Laboratory North Laurel, Maryland, United States)
Tony Colozza
(HX5, LLC)
Tom Packard
(HX5, LLC)
John Gyekenyesi
(HX5, LLC)
Brandon Klefman
(Glenn Research Center Cleveland, Ohio, United States)
Brent Faller
(Glenn Research Center Cleveland, Ohio, United States)
Natalie Weckesser
(Glenn Research Center Cleveland, Ohio, United States)
Onoufrios Theofylaktos
(Glenn Research Center Cleveland, Ohio, United States)
Christine Schmid
(Glenn Research Center Cleveland, Ohio, United States)
Chris Heldman
(Glenn Research Center Cleveland, Ohio, United States)
James Fittje
(Science Applications International Corporation (United States) McLean, Virginia, United States)
Ben Bussey
(Johns Hopkins University Applied Physics Laboratory North Laurel, Maryland, United States)
Paul Ostdiek
(Johns Hopkins University Applied Physics Laboratory North Laurel, Maryland, United States)
Tom Parkey
(Glenn Research Center Cleveland, Ohio, United States)
Cassandra Chang
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
August 29, 2022
Publication Date
October 1, 2022
Subject Category
Lunar And Planetary Science And Exploration
Spacecraft Design, Testing And Performance
Spacecraft Propulsion And Power
Report/Patent Number
CD-2021-182
E-20072
Funding Number(s)
WBS: 138494.01.99.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
DRPS
Dynamic Radioisotope Power System
Lunar Rover
VIPER
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