Estimation of Aero- and Aerothermo-Dynamic Characteristics for HTV-R

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概要

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• A series of aerodynamic tests have been conducted for the preliminary design of large scale recovery capsule HTV-R . Wind tunnel tests from low to hypersonic speeds and numerical analysis were conducted to establish the HRV aerodynamic database for the HTV-R's design. Experiments to improve testing and estimation capability of transonic dynamic stability characteristics, parachute characteristics at low speeds, and hypersonic RCS jet interaction were conducted for the development of the HTV-R program. This paper provides a summary of the objectives and scope of the aerodynamic tests.

• 特定非営利活動法人　日本ロケット協会の論文

著者

• MITSUO Kazunori

  Japan Society for the Promotion of Science (JSPS), DOMESTIC RESEARCH FELLOW Fluid Science Research C

• Fujita Kazuhisa

  Japan Aerospace Exploration Agency

• NAKAKITA Kazuyuki

  Japan Aerospace Exploration Agency, Chofu

• TANNO Hideyuki

  Japan Aerospace Exploration Agency, Kakuda

• TANNO Hideyuki

  Japan Aerospace Exploration Agency

• FUJII Keisuke

  Japan Aerospace Exploration Agency, Chofu

• NAKANO Eiichiro

  Japan Aerospace Exploration Agency, Tsukuba

• NAGAI Shinji

  Japan Aerospace Exploration Agency, Chofu

• IEMURA Kuniki

  IHI Aerospace Engineering

• TAKAMA Yoshiki

  Japan Aerospace Exploration Agency, Chofu

• MATSUYAMA Shingo

  Japan Aerospace Exploration Agency, Chofu

• MURAKAMI Keiichi

  Japan Aerospace Exploration Agency, Chofu

• MITSUO Kazunori

  Japan Aerospace Exploration Agency, Chofu

関連論文

• Numerical Simulation of Inductively Coupled Air Plasmas
• Temperature Correction of PSP Measurement Using Dual-Luminophor Coating
• Development of Shock Tube for Ground Testing Reentry Aerothermodynamics
• Near-Ultraviolet and Visible Spectroscopy of HAYABUSA Spacecraft Re-Entry
• An Overview of JAXA's Ground-Observation Activities for HAYABUSA Reentry
• Detection of Acoustic/Infrasonic/Seismic Waves Generated by Hypersonic Re-Entry of the HAYABUSA Capsule and Fragmented Parts of the Spacecraft
• Analysis of Shock Layer Radiation from the Vacuum-Ultraviolet to Near-Infrared Regions
• Shock Layer Radiation Analysis using a Hypervelocity Shock Tube (HVST)
• Numerical Analysis on the Nonequilibrium Phenomena of the Electronic Excitation Process behind Hypersonic Shock Waves
• Estimation of Aero- and Aerothermo-Dynamic Characteristics for HTV-R
• Water Landing Impact of Recovery Space Capsule: A Research Overview
• A Study of Thermal Protection System for HTV-R Reentry

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