Propulsion system for spacecraft
Number of patents in Portfolio can not be more than 2000
United States of America
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Dec 3, 2024
Grant Date -
May 18, 2023
app pub date -
Oct 9, 2020
filing date -
Oct 9, 2020
priority date (Note) -
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Abstract
A thrust generator is provided for producing thrust to move a spacecraft. The thrust generator includes a housing having a first end and an opposing second end. The first end is associated with a mount for coupling to the spacecraft. The housing further defines a central axis extending through the first end and the second end. The second end defines an annular propulsion outlet. At least one nozzle is positioned proximate the second end. The thrust generator is selectively operable in a first mode in which the thrust generator uses propellant to electrostatically generate thrust via the annular propulsion outlet, and a second mode in which the thrust generator uses propellant to gas-dynamically generate thrust via the at least one nozzle.
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