Exploring the Feasibility of Electrostatic Shielding for Spacecrafts
Author(s) -
Ram Tripathi,
John Wilson,
Robert C. Youngquist
Publication year - 2005
Publication title -
nasa technical reports server (nasa)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2005-6604
Subject(s) - electromagnetic shielding , spacecraft , electrostatic discharge , aerospace engineering , spacecraft charging , computer science , electrostatics , physics , engineering , electrical engineering , voltage , quantum mechanics
NASA is moving forward towards agency’s new vision for space exploration in the 21 st Century encompassing a broad range of human and robotic missions including missions to Moon, Mars and beyond. Exposure from the hazards of severe space radiation in deep space long duration missions is ‘the show stopper.’ Langley has developed state-of-the-art radiation protection and shielding technology for space missions. The payload penalty demands a very stringent requirement on the design of the spacecrafts for human deep space missions. The exploration beyond low Earth orbit (LEO) to enable routine access to more interesting regions of space will require protection from the hazards of the accumulated exposures of space radiation, Galactic Cosmic Rays (GCR) and Solar Particle Events (SPE), and minimizing the production of secondary radiation is a great advantage. There is a need to look to new horizons for newer technologies. The present investigation explores the feasibility of using the electrostatic shielding in concert with the innovative materials shielding and protection technologies. The asymmetries of the radiation shielding problem would be exploited in the electrostatics shielding process. The goal is to repel enough positive charge ions so that they miss the spacecraft without attracting thermal electrons. Conclusions are drawn about the advantages the electrostatic shielding, should it be successful, would bring to the radiation protection design process.
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