What is it about?
The rocket engine of the reusable sounding rocket was developed. This engine will be reusable for 100 flights and have high capabilities such as wide range continuous slottling , accurate controllability, and health monitoring. This paper describes 54 hot firing tests for this engine and numerical analysis for the chamber durability.
Featured Image
Read the Original
This page is a summary of: Development of a Reusable LOX/LH2 Rocket Engine - Firing Tests and Lifetime Evaluation Analysis, July 2015, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2015-4065.
You can read the full text:
Contributors
The following have contributed to this page
