The invention discloses a cone top cover pull type recovery sub-orbital carrier rocket, which belongs to the technical field of spaceflight rockets, and comprises a primary rocket body, a cone top cover arranged at the upper end of the primary rocket body, and a recovery power device, a load is accommodated in the cone top cover; the power recovery device at least comprises a power recovery engine and a power recovery cover arranged on the outer side of the power recovery engine, an engine jet pipe is arranged on the power recovery engine, and the orientation of the engine jet pipe is fixedly arranged or can be adjusted to be downward or outward obliquely downward; the two recovery power devices are symmetrically arranged on the outer side face of the upper portion of the first-stage rocket body or the outer side face of the cone top cover on the two sides. According to the cone top cover pull type recovery suborbital carrier rocket, the technical problems that in the prior art, a landing point is uncontrollable and recovery is difficult are solved, the test environment of ground launching, flight and suborbital flight can be provided, and an environment test in a real state and test services of the environment test can be provided for research and development of aerospace products.
本发明公开了一种锥顶罩拉式回收亚轨道运载火箭,其属于航天火箭技术领域,其包括一级箭体、设置于一级箭体上端的锥顶罩,以及回收动力装置;锥顶罩中容纳有载荷;回收动力装置至少包括回收动力发动机和设置于其外侧的回收动力罩,回收动力发动机上具有发动机喷管,发动机喷管的朝向固定设置为或可调节为向下或朝外的斜下方;回收动力装置有两个,于两侧对称地设置于一级箭体上部的外侧面上或者锥顶罩的外侧面上。本发明锥顶罩拉式回收亚轨道运载火箭解决了现有技术降落点不可控及回收有难度的技术问题,本发明能够提供地面发射、飞行及亚轨飞行的试验环境,可为空天产品的研制提供真实状态的环境试验及其试验服务。
Conical top cover pull type recycling sub-orbital carrier rocket
一种锥顶罩拉式回收亚轨道运载火箭
2022-07-12
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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