High Temperature Boost (HTB) Anode Power Supply for a Modular and Scalable Power Processing Unit

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作者
Carr, Gregory A. [1 ]
Iannello, Christopher J. [2 ]
Hunter, Don J. [1 ]
Lauenstein, Jean-Marie [3 ]
Ikpe, Stanley A. [4 ]
Ludwig, Lawrence L. [2 ]
Stell, Christopher [1 ]
Tuan Vo [1 ]
Del Castillo, Linda [1 ]
Weber, Carissa [1 ]
Mojarradi, Mohammad M. [1 ]
Orellana, Sonny [1 ]
Chen, Yuan [4 ]
机构
[1] CALTECH, Jet Prop Lab, 4800 Oak Grove Dr, Pasadena, CA 91109 USA
[2] NASA, Kennedy Space Ctr, Cocoa Beach, FL 32899 USA
[3] NASA, Goddard Space Flight Ctr, Greenbelt, MD 20771 USA
[4] NASA, Langley Res Ctr, Hampton, VA 23681 USA
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V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A 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.
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