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    • 60. 发明专利
    • Low wing monoplane delta wing supersonic rocket boat seaplane
    • JP2004082993A
    • 2004-03-18
    • JP2002291695
    • 2002-08-28
    • Jinichiro Ozawa小澤 甚一郎
    • OZAWA JINICHIRO
    • B64C35/00B64C30/00
    • PROBLEM TO BE SOLVED: To provide a low wing monoplane delta wing supersonic rocket boat seaplane reconstructed from a conventional model by facilitating landing and take-off of it with the whole of a main wing lower surface as a water touch-down bottom surface by a rocket and making it supersonic.
      SOLUTION: This low wing monoplane delta wing supersonic rocket boat seaplane is constituted by integrating a plurality of auxiliary rockets the jetting direction of which can be longitudinally, laterally and vertically changed with a delta wing boat seaplane with the whole of a main wing lower surface as the water touch-down bottom surface and the rocket boat seaplane constituted to be integrated with a rocket for launching of a space satellite. It is devised to climb steep by its main rocket, to metavertically take off and land on the water by the auxiliary rocket, to go out of the sphere of terrestrial gravitation by climbing steep while controlling its flight attitude in flight and to carry out supersonic inertial flight by inertia in the gravity-free and vacuum space. In the meantime, it is made to return to the earth by sufficiently reducing speed so that it is not heated even when it re-enters the atmosphere by reverse jetting of the auxiliary rocket and made to vertically land on the water even in the open sea in any stormy weather by making the jetting direction of the auxiliary rocket downward.
      COPYRIGHT: (C)2004,JPO