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Combination recovery rocket overall structure based on general core level

A combination and rocket technology, applied in the aerospace field, to optimize the force transmission path, improve the connection reliability, and achieve the effect of propellant management

Pending Publication Date: 2022-04-01
SHANGHAI AEROSPACE SYST ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In order to further enhance my country's ability to enter space, it is necessary to vigorously develop launch vehicle reuse technology. At present, there is a gap in the domestic reuse field.

Method used

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  • Combination recovery rocket overall structure based on general core level
  • Combination recovery rocket overall structure based on general core level
  • Combination recovery rocket overall structure based on general core level

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Embodiment Construction

[0029] In order to make the above objects, features and advantages of the present invention more comprehensible, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0030] Such as figure 1 As shown, the present invention provides a general configuration of recovery rocket based on a general-purpose core stage assembly, including the following components:

[0031] Core level one, including two level one liquid oxygen kerosene engines 22, one level heat shield 23, one level tail section 21, one level rear transition section 20, one level kerosene tank 18, one level inter-tank section 15, one level Liquid oxygen tank 14, grid rudder 13, first- and second-stage sections 11; among them, two first-stage liquid oxygen kerosene engines 22 are installed at the bottom of the first-stage tail section 21, work in a two-way swing mode, and have take-off and return deceleration 3 ignitions in the first an...

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Abstract

The invention provides an overall structure of an assembly recovery rocket based on a general core level. The overall structure comprises the following components of two first-stage liquid oxygen kerosene engines, a first-stage empennage, a first-stage tail section, a first-stage rear transition section, a first-stage kerosene tank, a first-stage inter-tank section, a first-stage liquid oxygen tank, a grid rudder and a second-stage inter-tank section. Two second-stage liquid oxygen kerosene engines, a second-stage kerosene tank, a second-stage tank interval section, a second-stage liquid oxygen tank, an instrument disc, a supporting cabin, an adapter and a belting connection unlocking device; each universal core-level booster comprises a nose cone, a grid rudder, a reaction thrust system, a liquid oxygen tank, an inter-tank section, a coal oil tank, a rear transition section, two liquid oxygen kerosene engines, a tail section and a landing buffer mechanism; front, middle and rear binding connection devices; a satellite fairing; the reverse thrust rocket is arranged between the first core stage and the booster box; and the forward thrust rocket and the reverse thrust rocket are arranged in the second-stage coal oil tank. According to the invention, general core-level assembly recovery is realized for the first time in China, an efficient and reliable assembly rocket recovery scheme is provided, the safety of a rocket falling area can be improved, and the rocket launching cost is greatly reduced.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to a return-type recovery rocket configuration based on a general-purpose core stage assembly. Background technique [0002] Entering space, using space and controlling space are the main tasks of aerospace forces, and entering space quickly and efficiently is the basis for using space and controlling space. As the main means of entering space at present, the development of launch vehicles has always been highly valued by the world's space powers, and puts forward higher requirements for new capabilities to enter space. In recent years, the rapid development of low-cost space access capabilities represented by repeated use has greatly reduced the cost of rocket launches. [0003] In order to further enhance my country's ability to enter space, it is necessary to vigorously develop launch vehicle reuse technology. At present, there is a gap in the domestic reuse field. Contents...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B15/00
Inventor 杨赧张锦朱亮聪宁国富杨帆张卫东洪刚张亮李红兵宋攀
Owner SHANGHAI AEROSPACE SYST ENG INST
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