Space Transportation FY2010 (January 20-21, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan
抄録（英）
Estimation of chamber pressure is necessary for the design of a hybrid rocket. Comprehension of combustion instability and regression rate behaviour is required in order to estimate chamber pressure. Characteristics of combustion instability and regression rate behaviour are called "internal ballistics". In this study, literature research of AIAA paper about hybrid rocket's internal ballistics is done to recognize technical problems of the evaluation of internal ballistics characteristic.
内容記述
形態: カラー図版あり
形態: CD-ROM1枚
内容記述（英）
Physical characteristics: Original contains color illustrations
Note: One CD-ROM
ハイブリッドロケット内部弾道特性評価技術の発展経緯と課題
