Investigation of Cryogenic Chilldown in a Complex Channel Under Low Gravity Using a Sounding Rocket
Author:
Affiliation:
1. University of Tokyo, Bunkyo, Tokyo 113-8656, Japan
2. Waseda University, Shinjuku, Tokyo 169-8555, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A34222
Reference21 articles.
1. Preliminary Study of High Power Hydrogen Electric Propulsion for the Space Exploration
2. Theoretical and experimental study of the active control of bubble point pressure using a magnetic field and its applications
3. Pulse Chilldown Tests of a Tank-to-Tank Liquid Hydrogen Propellant Transfer Line
4. Heat Exchange and Pressure Drop Enhanced by Sloshing
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