スポンサーリンク
Institute of Space and Astionautical Science, Japan Aerospace Exploration Agency | 論文
- Numerical Analysis of Sloshing and Wave Breaking in a Small Vessel by CIP-LSM(CIP)
- Thermal Responses of Ablator for Reentry Capsules with Superorbital Velocity
- An Experimental Study on the Boundary Layer Transition due to Gas Injection from Capsule-shape Body Surface
- Design Overview of an Asteroid 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