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High Temperature Boost (HTB) Anode Power Supply for a Modular and Scalable Power Processing UnitA concept of a modular and scalable 10kW to 80kW High Temperature Boost (HTB) Power Processing Unit (PPU) capable of operating at temperatures beyond the standard military temperature range was proposed for solar electric in-space propulsion. Within the PPU, the Anode Power Supply (APS) module is a 10kW modular power stage and is the key to the HTB PPU. This paper is to present the design, development, fabrication, testing and thermal demonstration of the 10kW HTB APS. The system architecture and the paradigm shift of the HTB PPU is also to be described. In addition, the extreme environments electronic and packaging technologies are addressed as the fundamental technology path. The HTB PPU is intended for power processing in the area of space solar electric propulsion, where reduction of in-space mass and volume are desired, and sometimes even critical, to achieve the goals of future space flight missions. The concept of the HTB PPU can also be applied to other extreme environment applications, such as geothermal and petroleum deep-well drilling, where higher temperature operation is required.
Document ID
20190025508
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Carr, Gregory A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Iannello, Christopher J.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Hunter, Don J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Lauenstein, Jean-Marie
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Ikpe, Stanley A.
(NASA Langley Research Center Hampton, VA, United States)
Ludwig, Lawrence L.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Stell, Christopher
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Vo, Tuan
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Castillo, Linda Del
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Weber, Carissa
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mojarradi, Mohammad M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Chen, Yuan
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
June 3, 2019
Publication Date
March 5, 2016
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
JPL-CL-16-0330
Report Number: JPL-CL-16-0330
Meeting Information
Meeting: IEEE Aerospace Conference
Location: Big Sky, MT
Country: United States
Start Date: March 5, 2016
End Date: March 12, 2016
Sponsors: Institute of Electrical and Electronics Engineers
Distribution Limits
Public
Copyright
Other

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