1995•Acta AstronauticaRequires access

Small body rendezvous mission using solar electric ion propulsion: Low cost mission approach and technology requirements

R. Kakuda, Joel Sercel, Wayne Lee

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Key concepts: Ion thruster, In-space propulsion technologies, Payload (computing), Rendezvous, Electrically powered spacecraft propulsion, Propulsion, Aerospace engineering, Spacecraft

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Small body rendezvous mission using solar electric ion propulsion: Low cost mission approach and technology requirements — Research Paper | ScholarLens