Power train for deep space solar electric propulsion
US10954005B1 · kind B1 · utility
Assignees
Inventors
Key dates
| Filing date | Jul 25, 2017 |
| Grant date | Mar 23, 2021 |
| Priority date | — |
| Expiry date | Dec 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.