Suborbital Reentry Demonstration of Inflatable Flare-Type Thin-Membrane Aeroshell Using a Sounding Rocket-Reference-Cited by-同舟云学术

Suborbital Reentry Demonstration of Inflatable Flare-Type Thin-Membrane Aeroshell Using a Sounding Rocket

Published:2015-01 Issue:1 Volume:52 Page:275-284
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Yamada Kazuhiko¹,Nagata Yasunori¹,Abe Takashi¹,Suzuki Kojiro²,Imamura Osamu³,Akita Daisuke⁴

Affiliation:

1. Department of Space Flight Systems, Japan Aerospace Exploration Agency, Kanagawa 252-5210, Japan

2. Department of Advanced Energy, The University of Tokyo, Chiba 277-8561, Japan

3. Department of Sustainable Engineering, Nihon University, Chiba 275-8575, Japan

4. Department of International Development Engineering, Tokyo Institute of Technology, Tokyo 152-8550, 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.A32807

Reference13 articles.

1. Survey of Ballute Technology for Aerocapture

2. GräßilinM.SchöttleU. “Flight Performance Evaluation of the Re-Entry Mission IRDT-1,” International Aeronautical Federation Paper IAF-01-v.3.05, Oct. 2001.

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

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

5. AndersonM. S.RobinsonJ. C.BushH. G.FralichR. W. “Tension Shell Structure for Application to Entry Vehicles,” NASA TN-D-2675, March 1965.

Cited by 37 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. Development of hybrid landing gear for OMOTENASHI surface probe;Acta Astronautica;2024-11

2. A three-dimensional thermochemical nonequilibrium model for simulating air plasma flows around an inflatable membrane reentry vehicle;Physics of Fluids;2024-08-01

3. Implementation of concavity over heat shield of a reentry vehicle in reducing aerodynamic heating;International Journal of Heat and Fluid Flow;2024-07

4. An open simulation model for terahertz wave transmission in plasma;Journal of Applied Physics;2024-04-17

5. Incremental model predictive control for satellite de-orbiting based on drag modulation;Acta Astronautica;2024-02