Development and simulation of a 3D printed liquid oxygen/liquid natural gas aerospike-Reference-Cited by-同舟云学术

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Development and simulation of a 3D printed liquid oxygen/liquid natural gas aerospike

Published:2024-03 Issue: Volume:216 Page:105-119
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Fadigati L.,Rossi F.,Souhair N.,Ravaglioli V.,Ponti F.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference69 articles.

1. Reusable launch vehicle propulsion based on the RD-0120 engine;Goncharov,1995

2. Experimental Study of Gas-Flow Separation in Overexpanded Exhaust Nozzles for Rocket Motors;Cowles,1949

3. Approximate method for plug nozzle design;Angelino;AIAA J.,1964

4. Annular Internal-External-Expansion Rocket Nozzles for Large Booster Applications;Connors,1961

5. Spike nozzle contour for optimum thrust;Rao;Planet. Space Sci.,1961

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Simulation of intra-chamber processes in a low-thrust rocket engine with a hydrogen-air mixture and counterflow cooling;Acta Astronautica;2024-12

2. Surface Pressure Measurement of Truncated, Linear Aerospike Nozzles Utilising Secondary Injection for Aerodynamic Thrust Vectoring;Aerospace;2024-06-24

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