Reusable two-stage injection aircraft with pneumatic combined structure connected in parallel

Abstract

The invention discloses a reusable two-stage injection aircraft with pneumatic combined structures connected in parallel, which comprises a booster-stage aircraft and a track-stage aircraft, a guide plane for mounting the track-stage aircraft is arranged on the upper surface of the booster-stage aircraft, and the guide plane is arranged along the length direction of booster-stage flight. And the guide plane is seamlessly attached to the lower surface of the orbit-level aircraft. According to the aerodynamic combined structure of the two-stage injection aircraft, the boosting-stage waverider base body and the orbit-stage waverider are constructed in a two-stage injection horizontal separation mode, and the aerodynamic layout of the deformable wings and the vertical tail rudder is added to the boosting-stage waverider base body, so that the aerodynamic combined structure of the two-stage injection aircraft has good wide-speed-range aerodynamic performance and stability performance; the technical risk of interstage separation is effectively reduced, and the method can be used as a scheme for transporting a reciprocating aircraft in the field of aerospace and can be repeatedly used.

Description

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AI Technical Summary

Benefits of technology

This patented technology allows for more flexibility when adjusting the wings' airfoil shape during flight or landing operations on different types of vehicles. It also includes an aerofoam that has been modified into multiple versions depending upon factors like altitude and wind conditions. Overall this makes flying drones safer from collateral damage caused due to high speeds while still being able to perform their tasks effectively without losing control over them.

Problems solved by technology

This patented describes a problem faced by both developing new type of space-based transport (SST) technology called Space Transport System(SVTS). Current methods require expensive engines like Rozers Power Augment), leading to increased costs and potential safety concerns. There is therefore a strong motivator behind research efforts towards creation of more efficient SSV technologies such as Multi Stage Track Intermediate Spatial Transfer Platforms (MISTPs).

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