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Credits:
Writer/Narrator: Brian McManus
Writer: Josi Gold
Editor: Dylan Hennessy
Animator: Mike Ridolfi
Animator: Eli Prenten
Sound: Graham Haerther
Thumbnail: Simon Buckmaster

References:
[1] “Increasing engine efficiency,” Aerospace America, Apr. 30, 2018. . https://aerospaceamerica.aiaa.....org/departments/incr
[2] “Falcon 9 - SpaceFlight Insider.” . https://www.spaceflightinsider.....com/hangar/falcon-9
[3] “Current State of NASA Continuously Rotating Detonation Cycle Engine Development,” in AIAA SCITECH 2023 Forum, American Institute of Aeronautics and Astronautics. https://arc.aiaa.org/doi/abs/10.2514/6.2023-1873
[4] “Computational Study of Deflagration to Detonation Transition in Pulse Detonation Engine Using Shchelkin Spiral,” Appl. Mech. Mater. https://www.scientific.net/AMM.772.136
[5] “A Theoretical Review of Rotating Detonation Engines | IntechOpen.” . https://www.intechopen.com/chapters/70511
[6] “Rotating detonation combustors and their similarities to rocket instabilities,” Prog. Energy Combust. Sci. https://www.sciencedirect.com/....science/article/abs/
[7] “Gaillard et al. - 2017 - Numerical simulation of a Rotating Detonation with.pdf.” . https://hal.science/hal-01558902/document
[8] “Teasley et al. - 2021 - A Review Towards the Design Optimization of High P.pdf.” . https://ntrs.nasa.gov/api/cita....tions/20210018267/do
[9] “Pressure Distribution and Performance Impacts of Aerospike Nozzles on Rotating Detonation Engines,” in 2018 AIAA Aerospace Sciences Meeting, Kissimmee, Florida, Jan. 2018, doi: 10.2514/6.2018-1626. https://arc.aiaa.org/doi/10.2514/6.2018-1626
[10] “Effect of Aerospike Plug Nozzle Design on Rotating Detonation Engine Performance for Rocket Applications | AIAA SciTech Forum.” . https://arc.aiaa.org/doi/abs/10.2514/6.2019-0197
[11] “観測ロケットS-520-31号機による深宇宙探査用デトネーションエンジン宇宙実証実験に成功,” 宇宙科学研究所. . https://www.isas.jaxa.jp/topics/002693.html
[12] “NASA RDRE For Release to AIAA Teasley ER13.pdf.” . https://ntrs.nasa.gov/api/cita....tions/20220012375/do

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