Static Engine Test on CTN Model Rocket Engine with 1/2 A6-2 Propellant
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-99-4758-4_21
Reference19 articles.
1. Nazri M, Jaafar m (2014) Development of solid rocket propulsion system at UTM
2. Kuo KK (ed) (1984) Fundamentals of solid-propellant combustion. American Institute of Aeronautics and Astronautics
3. Williams FA, Barrère M, Huang NC (1969) Fundamental aspects of solid propellant rockets. Advisory group for aerospace research and development Neuilly-Sur-Seine (France)
4. Schüttauf K et al (2016) Operation of solid rockets in comparison with hybrid rockets during the STERN project. SpaceOps 2016 conference, 13 May 2016. https://doi.org/10.2514/6.2016-2613
5. Beckstead MW, Derr RL, Price CF (1970) A model of composite solid-propellant combustion based on multiple flames. AiAA J S(12):2200–2207
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