The Development of a Control System for a 5 Kilowatt Free Piston Stirling Space Convertor
Author(s) -
Raymond L. Kirby,
N. Vitale,
Mohamed S. ElGenk
Publication year - 2008
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.177
H-Index - 75
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/1.2844988
Subject(s) - setpoint , stirling engine , piston (optics) , engineering , control system , automotive engineering , electrical engineering , computer science , mechanical engineering , physics , wavefront , artificial intelligence , optics
The new NASA Vision for Exploration, announced by President Bush in January 2004, proposes an ambitious program that plans to return astronauts to the moon by the 2018 time frame. A recent NASA study entitled “Affordable Fission Surface Power Study” recommended a 40 kWe, 900 K, NaK‐cooled, Stirling conversion for 2020 launch. Use of two of the nominal 5 kW converters allows the system to be dynamically balanced. A group of four dual‐converter combinations that would yield 40 kWe can be tested to validate the viability of Stirling technology for space fission surface power systems. The work described in this paper deals specifically with the control system for the 5 kW convertor described in the preceding paragraph. This control system is responsible for maintaining piston stroke to a setpoint in the presence of various disturbances including electrical load variations. Pulse starting of the FSPE convertor is also an inherent part of such a control system. Finally, the ability to throttle the engine to mat...
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