Trajectory Estimation of the Hayabusa Spacecraft During Atmospheric Disintegration-Reference-Cited by-同舟云学术

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Trajectory Estimation of the Hayabusa Spacecraft During Atmospheric Disintegration

Published:2013-03 Issue:2 Volume:50 Page:326-336
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Shoemaker Michael A.¹,van der Ha Jozef C.²,Abe Shinsuke³,Fujita Kazuhisa⁴

Affiliation:

1. Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 819-0395, Japan

2. Mission Design and Operations, Deming, Washington 98244

3. National Central University, Taoyuan 32001, Taiwan, Republic of China

4. Japan Aerospace Exploration Agency, Kanagawa 229-8510, 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.A32338

Reference62 articles.

1. An Overview of JAXA's Ground-Observation Activities for HAYABUSA Reentry

2. Airborne Observation of the Hayabusa Sample Return Capsule Re-entry

3. Trajectory reconstruction of Hayabusa's atmospheric reentry

4. Overview of entry risk predictions

5. BouslogS.RossB.MaddenC. “Space Debris Reentry Risk Analysis,” AIAA Paper 1994-0591, 1994.

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