NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Continued Development of the Advanced Stirling Convertor (ASC)The Advanced Stirling Convertor (ASC) is being developed under contract with the NASA Glenn Research Center (GRC) and is supported by NASA s Science Mission Directorate for potential use in future radioisotope power systems having significantly increased efficiency and higher specific power compared to the current thermoelectric systems. An ASC with a lower temperature (approx.650 C) Inconel heater head is currently being substituted into the DOE/Lockheed Martin Advanced Stirling Radioisotope Generator (ASRG) program with a predicted convertor efficiency of 34 percent (AC electrical out to heat input ) at a temperature ratio of 2.7 and is expected to deliver approximately 75 W(sub ac). Continued development of the higher temperature (approx.850 C) version using existing materials and fabrication techniques in the hot portions is reported on here. The higher temperature ASC is expected to have 38 percent efficiency (AC electrical out to heat input) at a temperature ratio of 3.1 and is expected to deliver approximately 88 W(sub ac). The high temperature ASC also has approximately 30 C higher rejection temperature, which allows for further reduced system mass because of the reduced radiator size. Six higher temperature and hermetically sealed convertors are being built under this effort for extended life testing at GRC.
Document ID
20090007962
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Wong, Wayne A.
(NASA Glenn Research Center Cleveland, OH, United States)
Wood, J. Gary
(SunPower, Inc. Athens, OH, United States)
Wilson, Kyle
(SunPower, Inc. Athens, OH, United States)
Buffalino, Andrew
(SunPower, Inc. Athens, OH, United States)
Frye, Patrick
(Pratt and Whitney Rocketdyne Canoga Park, CA, United States)
Matejczyk, Dan
(Pratt and Whitney Rocketdyne Canoga Park, CA, United States)
Penswick, L.B.
(Consultant Stevenson, Washington, USA)
Date Acquired
August 24, 2013
Publication Date
December 1, 2008
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-16192
NASA/TM-2008-215021
Funding Number(s)
CONTRACT_GRANT: NAS3-03128
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available