Propulsion system for spacecraft
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.
1. A thrust generator for producing thrust to move a spacecraft, the thrust generator comprising:
a housing having a first end and an opposing second end, the first end associated with a mount for coupling to the spacecraft, the housing further defining a central axis extending through the first end and the second end, the second end defining an annular propulsion outlet;
a tube extending through the housing from the first end to the second end and positioned concentrically with the central axis; and
a nozzle fluidly connected to the tube,
wherein 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 nozzle.
2. The thrust generator of claim 1 , wherein the nozzle is positioned at an end of the tube.
3. The thrust generator of claim 1 , wherein the annular propulsion outlet and nozzle are configured such that a resultant thrust generated in the first mode and a resultant thrust generated in the second mode are both effectively coaxial along the central axis.