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Heavy carrier rocket

A carrier rocket and heavy-duty technology, applied in the direction of rocket engine devices, weapon types, jet propulsion devices, etc., to achieve the effect of easy use and clear structure

Inactive Publication Date: 2021-11-19
冯国彦
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the process of research and development and launch of the launch vehicle, there are some problems in efficiency, energy consumption, speed, height, etc.

Method used

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  • Heavy carrier rocket
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Embodiment Construction

[0019] The technical solutions of the present invention will be clearly and completely described below in conjunction with the accompanying drawings. Apparently, the described embodiments are part of the embodiments of the present invention, but not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0020] In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", The orientation or positional relationship indicated by "front", "back", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the manner or the original must have Certai...

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Abstract

The invention discloses a heavy carrier rocket which comprises a first-stage power body, a second-stage power body and a third-stage power body, and an effective load body is arranged at the top of the third-stage power body; an escape tower, an instruction cabin and a service cabin are arranged in the effective load body; an instrument bin, a third-stage liquid oxygen tank, a third-stage liquid hydrogen tank and a third-stage engine are arranged in the third-stage power body; a second-stage liquid oxygen tank, a second-stage liquid hydrogen tank and a second-stage engine are arranged in the second-stage power body; and the first-stage power body internally comprises a first-stage liquid oxygen tank, a first-stage coal oil tank, a first-stage reaction transition section and a first-stage tail section which are sequentially arranged from top to bottom, a first-stage engine is arranged in the first-stage tail section, and a stable tail wing is arranged on the outer side of the first-stage tail section. Compared with the prior art, the heavy carrier rocket has the advantages that the heavy carrier rocket is clear in structure and convenient to use, the multi-stage structure is adopted, different propellants are adopted among multiple stages to be matched with a corresponding high-pressure afterburning engine for propelling, and therefore the lift-off and lunar landing of the heavy carrier rocket are achieved.

Description

technical field [0001] The invention relates to the technical field of rockets, in particular to a heavy-duty launch vehicle. Background technique [0002] In 2014, my country officially announced that private enterprises were allowed to build and launch satellites, which stimulated the enthusiasm of domestic private capital to participate in the aerospace industry and accelerated the development of the domestic small satellite industry. Subsequently, commercial rocket technology is also booming, especially solid multi-stage launch vehicle technology. Due to the relatively low threshold, many commercial solid multi-stage launch vehicles have been successfully launched in recent years. In the process of research and development and launch of the launch vehicle, there are some problems in efficiency, energy consumption, speed, height, etc. [0003] Therefore, a heavy-duty launch vehicle needs to be studied urgently. Contents of the invention [0004] The purpose of the pre...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B15/00F02K9/42
CPCF42B15/00F02K9/42F02K9/425
Inventor 冯国彦
Owner 冯国彦