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IHI Aerospace Company | 論文
- Thermal Responses of Ablator for Reentry Capsules with Superorbital Velocity
- System Description and Reentry Operation Scenario 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