REENTRY DYNAMICS OF MUSES-C
スポンサーリンク
概要
著者
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Ishii Nobuaki
The Institute Of Space And Astronautical Science Jaxa
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Yamada Tetsuya
The Institute Of Space And Astronautical Science Jaxa
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Hinada Motoki
Ihi Aerospace Company
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HIRAKI Koju
Kyushu Institute of Technology
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INATANI Yoshifumi
The Institute of Space and Astronautical Science, JAXA
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HIRAKI Koju
The Institute of Space and Astronautical Science
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MAKINO Takashi
Nissan Motor Co., Ltd.
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HONDA Masahisa
Nissan Motor Co., Ltd.
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Inatani Y
The Institute Of Space And Astronautical Science Jaxa
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Makino Takashi
Nissan Motor Co. Ltd.
関連論文
- Alumina Particles Exhausted from Soild-Propellant Rocket Motor As a Potential Source of Space Debris
- Reentry Motion and Aerodynamics of the MUSES-C Sample Return Capsule
- System Description and Reentry Operation Scenario of MUSES-C Reentry Capsule
- Attitude Motion and Aerodynamic Characteristics of MUSES-C Reentry Capsule
- A Unique Single Stage Parachute System and Qualification by Balloon Drop Tests
- Thermal Protection System of the Reentry Capsule with Superorbital Velocity
- REENTRY DYNAMICS OF MUSES-C
- An Arc-Heated High Enthalpy Test Facility for Thermal Protection Studies
- Separated flow around a rotating gyroball
- Design of Particle/Granules Damper for Vertical Vibration with Approximate Analysis