Effect of Different Injectors on Performance of Hybrid Rocket Motor by Varying the L/D Ratio
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-97-1306-6_23
Reference18 articles.
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3. Mazzetti A, Merotto L, Pinarello G (2014) Paraffin-based hybrid rocket engines applications: a review and a market perspective. Acta Astronaut 126:286–297
4. Okninski A (2018) On use of hybrid rocket propulsion for suborbital vehicles. Acta Astronaut 145:1–10
5. Cai G, Zhu H, Rao D, Tian H (2013) Optimal design of hybrid rocket motor powered vehicle for suborbital flight. Aerosp Sci Technol 25(1):114–124
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