The invention provides a reusable horizontal take-off and landing two-stage aerospace vehicle. A first-stage structure is a reusable winged sub-orbital aircraft, and the whole aircraft is of an aerospace aircraft structure; and the second-stage structure is a traditional rocket structure. Wherein the first stage can realize horizontal rising and landing, and the second stage adopts a recovery scheme of maritime splashing recovery. The aircraft can be recycled and reused while efficient carrying is ensured.
本发明提供一种可重复使用的水平起降二级空天运载器,一级结构为可重复使用的带翼亚轨道飞行器,整体为空天飞机构型;二级结构为传统火箭构型。其中一级可实现水平起降,二级采用了海上溅落回收的回收方案。本发明在确保高效运载的同时实现飞行器回收和可重复使用。
Reusable horizontal take-off and landing two-stage aerospace vehicle
一种可重复使用的水平起降二级空天运载器
2024-07-12
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
Reusable vertical take-off and landing space launch vehicle
European Patent Office | 2020
|Prospects for the Advancements of Reusable Aerospace Transportation Systems with Horizontal Take-Off
British Library Conference Proceedings | 1994
|Predefined-time control for a horizontal takeoff and horizontal landing reusable launch vehicle
Emerald Group Publishing | 2021
|