Numerical comparison of exhaust plume flow behaviors of small monopropellant and bipropellant thrusters

Author:

Lee Kyun HoORCID

Funder

Ministry of Science, ICT and Future Planning

Publisher

Public Library of Science (PLoS)

Subject

Multidisciplinary

Reference20 articles.

1. Aerojet Rocketdyne (2016) Monopropellant rocket engines. http://www.rocket.com/propulsion-systems/monopropellant-rockets.

2. Airbus Safran Launchers GmbH (2016) 4 N bipropellant thruster. http://www.space-propulsion.com/spacecraft-propulsion/bipropellant-thrusters/4n-thruster.html.

3. Plume flow and plume impingement in space technology;G Dettleff;Prog Aerosp Sci,1991

4. Grabe M, Boettcher RD, Fasoulas S, Hannemann K. Numerical simulation of nozzle flow into high vacuum using kinetic and continuum approaches. 16th STAB/DGLR Symposium, Aachen, Germany; 2008.

5. Molecular gas dynamics and the direct simulation of gas flows;GA Bird,1992

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