Design and analysis of an additively manufactured rotating detonation rocket engine chamber for calorimetry and thermal management assessment-Reference-Cited by-同舟云学术

Design and analysis of an additively manufactured rotating detonation rocket engine chamber for calorimetry and thermal management assessment

Published:2023-01-19 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2023 Forum
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Author:

Hernandez-McCloskey Joseph¹,Pineda Daniel I.¹,Bennewitz John W.²,Bigler Blaine R.³,Burr Jason R.⁴,Danczyk Stephen A.⁴,Paulson Eric J.⁴,Hargus William A.⁴

Affiliation:

1. The University of Texas at San Antonio

2. The University of Alabama in Huntsville

3. Jacobs Technology Inc.

4. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2023-0355

Reference17 articles.

1. To the Question of Energy Use of Detonation Combustion

2. Air Force Research Laboratory Rotating Detonation Rocket Engine Development

3. Injector Mixing Effects in Rotating Detonation Rocket Engines

4. Kirchberger, C. "Investigation on Heat Transfer in Small Hydrocarbon Rocket Combustion Chambers," Ph.D. thesis,2014.

5. Quentmeyer, R. J., and Roncace, E. A. "Hot-Gas-Side Heat Transfer Characteristics of Subscale, Plug-Nozzle Rocket Calorimeter Chamber," Tech. Rep. NASA-TP-3380, National Aeronautics and Space Administration Lewis Research Center, Cleveland, OH, 1993.

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