A Short Review on Efficiency of Rotating Detonation Engine

Authors

DOI:

https://doi.org/10.61359/11.2106-2310

Keywords:

Aerospace, Rotating Detonation Enginer, RDE, PDE, Pulse Detonation Enginer

Abstract

The rotating detonation engine (RDE) is a revolutionary propulsion technology with the potential to significantly enhance the efficiency of propulsion systems. This paper provides an in-depth review of the RDE's efficiency, its advantages over pulse detonation engines (PDEs) and deflagration concepts, as well as its applications in rocketry. The historical development of detonation engines, specifically RDE, is discussed, along with various research methodologies applied in both atmospheric and vacuum conditions. The challenges and potential solutions for utilizing RDE in space missions are also explained in this paper.

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Author Biography

Lalith Veeramanikandan, Intern, Acceleron Aerospace, Bangalore, Karnataka, India - 560037

Lalith Veeramanikandan, an Aerospace Intern at Acceleron Aerospace, is a driven figure from Karaikudi, Tamil Nadu, and India. With an ardent interest in Aerospace Propulsion and RDE Engines, he navigates intricate aerospace innovations. Lalith's focus on the transformative Rotating Detonation Engine (RDE) technology showcases his attention to detail and determination to enhance propulsion efficiency. His research extends to broader aerospace domains, reflecting his commitment to shaping the future of space exploration. Rooted in Karaikudi, Lalith's journey epitomizes dedication to aerospace advancement, making him a notable contributor to the field's evolution.

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Published

2023-08-30

How to Cite

Veeramanikandan, L. (2023). A Short Review on Efficiency of Rotating Detonation Engine. Acceleron Aerospace Journal, 1(2), 44–46. https://doi.org/10.61359/11.2106-2310

Issue

Vol. 1 No. 2 (2023): Launching the Future: Charting the Course for Aerospace Excellence in the Second Issue of Acceleron Aerospace Journal

Section

Articles

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License

Copyright (c) 2023 Lalith Veeramanikandan

Creative Commons License

This work is licensed under a Creative Commons Attribution 4.0 International License.

The Acceleron Aerospace Journal, with ISSN 2583-9942, uses the CC BY 4.0 International License. You're free to share and adapt its content, as long as you provide proper attribution to the original work.