A Design Method for Horizontal Stage Separation of Parallel Dual Waverider Two-stage Orbiting Vehicle

Abstract

The invention discloses a design method for the horizontal inter-stage separation of a parallel double waverider two-stage orbiting aircraft, which includes constructing an assembly structure of an orbital-level waverider aircraft and a booster-level waverider aircraft; in the assembly When the flight of the structure reaches the separation condition between the stages, the lift force on the two wings of the booster stage waverider aircraft will be unbalanced, and then the combined structure will roll 90° around the fuselage laterally; Under the roll of 90°, the orbital-level waverider aircraft performs a horizontal separation action along the upper surface of the booster-level waverider aircraft under its own power; after the orbital-level waverider aircraft separates from the booster-level waverider aircraft, it continues to Roll 90° in the direction and climb to the target orbit, and the booster-stage waverider vehicle rolls 90° in the opposite direction to restore the initial flight state, realizing the separation between the two horizontal stages. The horizontal interstage separation method of the present invention avoids the problems of high pressure, high heat flow and stability in conventional separation processes under hypersonic conditions.

Description

technical field [0001] The invention relates to the field of aviation technology, in particular to a design method for separating the horizontal stages of a parallel double waverider two-stage orbiting aircraft. Background technique [0002] The two-stage orbiting vehicle has been extensively studied as the next-generation reusable space-to-ground transportation system with low cost, high efficiency, and high reliability. The horizontal take-off and landing two-stage orbiter consists of an air-breathing powered booster stage and a reusable rocket-powered orbital stage. Horizontal take-off and landing two-stage orbiting aircraft generally carry the orbital stage on the back of the booster stage to take off at a conventional airport. , the booster stage maneuvers and controls to return to the airport by itself, and the orbital stage accelerates to climb into orbit under the propulsion of the rocket. After completing the orbital mission, the orbital stage glides back to land. ...

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a design method for the horizontal separation of the parallel dual waverider two-stage orbiting aircraft to solve the technical problem of the horizontal separation of the parallel dual waverider aircraft in the prior art

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