Patent · US Active

Power train for deep space solar electric propulsion

US10954005B1 · kind B1 · utility

0Cited by
6References
20Claims
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Key dates

Filing dateJul 25, 2017
Grant dateMar 23, 2021
Priority date
Expiry dateDec 20, 2039

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG05F1/67
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

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, Vi; and delivers power to the electric propulsion subsystem at a voltage, Vo. The spacecraft is configured to operate at a varying distance, D, from the sun within the range of Dmin to Dmax, Dmax being at least 1.3×Dmin. The solar array is configured to deliver power to the power conversion module at a voltage approximately equal to Vo when the spacecraft is proximate to Dmax.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.