Performance aspects of plug cluster nozzles
Author:
Affiliation:
1. Technical University of Munich, Munich 80333, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26792
Reference17 articles.
1. Spike nozzle contour for optimum thrust
2. Design of Maximum Thrust Plug Nozzles for Fixed Inlet Geometry
3. The design of linear aerospike thrust cells
4. Thrust cell technology for modular engines
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