The
spacecraft structure is provide, the
spacecraft structure for the
spacecraft includes, a center
fuselage, right wing side
fuselage, left wing side
fuselage, front wings, and rear wings of Arch-Wings, vertical winglets, and the first levels, the fuselage has a cross-section of substantially flat floor fuselage shape, being is wide enough to provide lifting force.The front wings of the Arch-Wings are disposed horizontally in rear portions of the fuselage the vertical winglets are disposed the top of the rear fuselage the first level disposed
fuel tank storage, plurality of
landing gear bays,
cockpit with control panel, various avionic instruments, cabin
doors.The top of the rear fuselage disposed jet-power plants and further more at compartment of the Arch-Wings disposed
rocket power plants.The fuselage provide lifting force and the wings provides lifting force and steering force, he whole structure of spacecraft comprises carbon
fiber honey comb composite molded structure which is makes the spacecraft lighter weight and shear strong.At the front portion of wing
body compartment of the Arch-Wings comprises retro
rocket power
plant with covered door, and under belly of the Arch-Wings disposed pontoon systems which could provide float at sea port.