Approaches to actively protect spacecraft from damage due to...

Aeronautics and astronautics – Spacecraft – With shield or other protective means

Reexamination Certificate

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Reexamination Certificate

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07637461

ABSTRACT:
A method whereby one or more conducting plates electrically-biased negatively with respect to a spacecraft's electrical potential and insulated from the spacecraft surface are located around the spacecraft surface whereby contaminant ions in a plasma surrounding the spacecraft are attracted to and accelerated through the conducting plates electric potential, caused to collide with the conductive surface, neutralized through collisions with surface atoms, and then reflected away from the spacecraft as neutral atoms or molecules.

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patent: 5488372 (1996-01-01), Fischer
patent: 5962850 (1999-10-01), Wuest
patent: 6332590 (2001-12-01), Oh
patent: 6362574 (2002-03-01), Aguero et al.
patent: 6683311 (2004-01-01), Wuest
patent: 2190544 (1987-11-01), None
Cuthbertson, J. W. et al, “High-flux source of low-energy neutral beams using reflection of ions from metals,” Rev. Sci Instrum. 63 (11) Nov. 1992.
Hagstrum, H. D., “Reflection of Noble Gas Ions at Solid Surfaces,” Phy. Rev. vol. 123, No. 3, Aug. 1, 1961.

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