ハイブリッドロケット用デルタ翼の空力特性(S68-3 ハイブリッドロケットおよび回収技術,S68 学生による宇宙活動)

概要

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The winged-vehicle for the fly-back system of CAMUI (CAscaded Multistage Impinging-jet) hybrid-rocket has been developed. As the first stage, we carried out the gliding test of a Space-shuttle type winged-vehicle. In the test, the winged-vehicle was carried by a radio-controlled airplane, separated, glided and landed. Then, we conducted a launching test using model rocket engine. The results encouraged us to proceed to further development of the fly-back system. As the second stage, we carried out the tests to develop the delta wing assembled to, CAMUI hybrid-rocket. In the wind tunnel test, the aerodynamic characteristics of the delta wing were investigated. Also, the flight performance of the delta wing was checked by the water-rocket test. These results provided useful data to design and make a delta wing of optimal shape. The present results led to the success of the fly-back test of CAMUI hybrid rocket.
社団法人日本機械学会の論文
2004-09-04