Comparison of flight and shock tunnel spectroscopy of Hayabusa2 Sample Return Capsule
Author:
Affiliation:
1. Uchu Koku Kenkyu Kaihatsu Kiko
2. Mobile Aerospace Reconnaissance Systems Scientific, Inc.
3. NASA Ames Research Center
4. Torch Technologies Inc, Torch Technologies Inc, Huntsville, AL, US, corporate/consult
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-3734
Reference18 articles.
1. Kitazono, K., Takahashi, M., Ohnishi, N. and Tanno, H, "Numerical Study of Unsteady High Enthalpy Flow in an Expansion Tube", AIAA Paper No.2019-1392, AIAA SciTech 2019 Forum, https://doi.org/10.2514/6.2019-1392
2. Sakai, T., Takami, H., and Tanno, H. "Calculation of Strong Shock Wave Propagation in an Expansion Tube", AIAA Paper No.2020-1709, AIAA SciTech 2020 Forum, https://doi.org/10.2514/6.2020-1709 [7] https://airbornescience.nasa.gov/category/Mission/SHARC
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