Experimental and numerical investigation of swirling H2O2 and polypropylene hybrid rocket motor with regenerative cooling

Author:

Li M.-C.,Wei S.-S.,Hung C.-H.,Wu J.-S.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference24 articles.

1. Alessandro Ruffin, Enrico Paccagnella, Marco Santi, Francesco Barato, Daniele Pavarin, Real time deep throttling tests of a hydrogen peroxide hybrid rocket motor, in: AIAA Propulsion and Energy 2019 Forum, Indianapolis, IN, 2019.

2. Nano/Microsatellite Market Forecast;Doncaster,2017

3. Martina G. Faenza, Adrien J. Boiron, Bastien Haemmerli, Solli Lennart, Terje Vesterås, Onno Verberne, Getting ready for space: Nammo’s development of a 30 kN hybrid rocket based technology demonstrator, in: EUCASS2017, Norway, 2017.

4. A. Karabeyoglu, E. Toson, B. Evans, O/F shift in hybrid rockets, in: 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cleveland, OH, 2014.

5. Experimental study of the swirling oxidizer flow in HTPB/N2O hybrid rocket motor;Heydari;Int. J. Aerosp. Eng.,2017

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