Aerodynamic Heating Around Flare-Type Membrane Inflatable Vehicle in Suborbital Reentry Demonstration Flight-Reference-Cited by-同舟云学术

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Aerodynamic Heating Around Flare-Type Membrane Inflatable Vehicle in Suborbital Reentry Demonstration Flight

Published:2015-11 Issue:6 Volume:52 Page:1530-1541
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Takahashi Yusuke¹,Yamada Kazuhiko²,Abe Takashi²,Suzuki Kojiro³

Affiliation:

1. Faculty of Engineering, Hokkaido University, Hokkaido 060-8628, Japan

2. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Kanagawa 252-5210, Japan

3. Graduate School of Frontier Sciences, The University of Tokyo, Chiba 277-8561, 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.A33170

Reference26 articles.

1. Inflatable Re-entry Vehicle Experiment (IRVE) Design Overview

2. Survey of Ballute Technology for Aerocapture

3. Postflight Analysis of Inflatable Reentry and Descent Technology Blackout During Earth Reentry

4. Hypersonic Inflatable Aerodynamic Decelerator (HIAD)Technology Development Overview

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4. Numerical investigation of surface catalytic effect on the plasma sheath of a hypersonic re-entry capsule;Physics of Fluids;2023-05-01

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