High-diodicity impinging injector design for rocket propulsion enabled by additive manufacturing
Author:
Affiliation:
1. University of California Los Angeles
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-1265
Reference11 articles.
1. Minimizing hydraulic losses in additively manufactured swirl coaxial injectors
2. A Review Towards the Design Optimization of High Performance Additively Manufactured Rotating Detonation Rocket Engine Injectors
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