California Institute of Technology

Space Systems/loral, LLC

Gregory Alan Carr

Dan M Goebel

Peter W Lord

David Younghee Oh

Bao Hoang

Christopher Bryan Stell

Jorge Delgado

Lee Charles Rotlisberger

Denis Trofimov

A spacecraft includes a power train that includes a solar array, an electric propulsion subsystem, and a power conversion module. The power conversion module receives power from the solar array at a voltage, V; and delivers power to the electric propulsion subsystem at a voltage, V. The spacecraft is configured to operate at a varying distance, D, from the sun within the range of Dto D, Dbeing at least 1.3&#xd7;D. The solar array is configured to deliver power to the power conversion module at a voltage approximately equal to Vwhen the spacecraft is proximate to D.

Power train for deep space solar electric propulsion

Growing community of inventors

Agua Dulce, CA, United States of America

Gregory Alan Carr