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A rocket propulsion system for spacecraft achieves greater economy, reliability and efficiency rocket by incorporating monopropellant RCS thrusters (1a-1f) for attitude control and bipropellant SCAT thrusters (5a-5c) for velocity control. Both sets of thrusters are designed to use the same liquid fuel, supplied by a pressurized non-pressure regulated tank, and operate in the blow down mode.
A new propulsion system is proposed and a new bi-propellant thruster construction is described that has dual mode capability. That thruster construction is presently referred to as a Secondary Combustion Augmented Thrusters or, simply, as a "SCAT" thruster.
This is not the only site referencing this thruster. I have encountered indications this is a relatively recent application. Comments? ☉Qψîδịzഴⓧ•—>Quisizyxtalk22:05, 7 May 2021 (UTC)[reply]
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