NASA NTRS · 19720000501
Integrated monopropellant thruster
Abstract
Application of vortex amplifier principles to throttling of monopropellant thrusters is described. Integration of flow control, catalyst bed, and thruster nozzle is accomplished by design of thruster. Diagrams of thrusters are provided to show details of construction and operation.
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Mangion, C.. 1972-08-01. Integrated monopropellant thruster. https://ntrs.nasa.gov/citations/19720000501
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