Aerodynamic evaluation of a capsule shaped projectile during free flight testing with ballistic range

Akiho Ishida, Hiroki Nagai, Hideyuki Tanno, Tomoyuki Komuro

研究成果: Conference contribution

2 被引用数 (Scopus)

抄録

The HTV Return Vehicle (HRV) has been considered the initial model of the first manned re-entry capsule by Japan Aerospace Exploration Agency. The aerodynamic characteristics must be clarified for stable parachute deployment and landing because the blunt body is generally brought to dynamic instability at transonic and subsonic flows. In this study, free flight tests of an HRV shaped projectile were conducted in a ballistic range owned by JAXA Kakuda Space Center. The projectile motion during free flight was measured by the onboard four accelerometers. From the results, angular rate and angle time history were calculated. A method for constructing the motion model was developed, and we concluded that the projectile was in dynamic instability in some periods. Finally, a method for the rejection of the deceleration effect in free flight testing was proposed.

本文言語English
ホスト出版物のタイトル53rd AIAA Aerospace Sciences Meeting
出版社American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN(印刷版)9781624103438
DOI
出版ステータスPublished - 2015
イベント53rd AIAA Aerospace Sciences Meeting, 2015 - Kissimmee, United States
継続期間: 2015 1 52015 1 9

出版物シリーズ

名前53rd AIAA Aerospace Sciences Meeting

Other

Other53rd AIAA Aerospace Sciences Meeting, 2015
国/地域United States
CityKissimmee
Period15/1/515/1/9

ASJC Scopus subject areas

  • 航空宇宙工学

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