NASA NTRS · 19820010440
Low thrust monopropellant engine
Abstract
The engine has a conventional body and nozzle configuration. The monopropellant fuel is fed into the thruster with dual injection tubes via an injector shell with dual spray jets. The spray jets are positioned generally opposed to each other. A heater screen pack combination thermally decomposes the fuel after injection into the combustion chamber of the thruster.
Keep this discovery
Explore connections, maps & timelines
Kuenzly, J. D.. 1981-09-15. Low thrust monopropellant engine. https://ntrs.nasa.gov/citations/19820010440
Cite the original work for its findings. Save a collection to share your selection of sources.