Geometrical characterization and performance optimization of monopropellant thruster injector

Author:

Nada T.R.,Hashem A.A.

Publisher

Elsevier BV

Subject

General Earth and Planetary Sciences

Reference18 articles.

1. Transient behavior of H2O2 thruster: effect of injector type and ullage volume;An;Journal of Propulsion and Power,2009

2. Chugging instability of H2O2 monopropellant thrusters with reactor aspect ratio and pressures;An;Journal of Propulsion and Power,2011

3. Liquid Atomization;Bayvel,1993

4. Theoretical formulation for Sauter Mean Diameter of pressure-swirl atomizers;Couto;Journal of Propulsion and power,1997

5. Darina, J., Michal, K., Tadeáš, L., Václav, K., 2011. The Study of Full Cone Spray Using Interferometric Particle Imaging Method, Experimental Fluid Mechanics Conference, EFM11, 2011, Jicín, Czech Republic.

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1. Effects of geometric parameters on flow and atomization characteristics of swirl nozzles for artificial snowmaking;International Journal of Refrigeration;2023-10

2. Conceptual Design of Small-Sized Thruster Using Laser Ignition of High-Energy Monopropellant;Journal of Propulsion and Power;2023-05

3. Study on inlet pressure and Reynolds number in pressure-swirl atomizer with spiral path;International Communications in Heat and Mass Transfer;2022-10

4. Experimental investigation on fluid structure and full-cone spray characteristics of a jet-swirl atomizer using shadowgraph technique;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-08-11

5. Numerical investigation of the full-cone spray structure and characteristics provided by a jet-swirl atomizer;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2019-07-01

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