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A rocket fairing recovery system and method

A technology of recovery system and fairing, which is applied in the field of rocket fairing recovery system, can solve the problems of poor maneuverability and high difficulty of recovery, and achieve the effect of reducing the difficulty of recovery, reliable connection and fast connection

Active Publication Date: 2021-08-03
BEIJING XINGJI RONGYAO SPACE TECH CO LTD +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the maneuverability of the receiving ship at sea is poor, and the fairing is in seawater, requiring a short soaking time before it can be reused, so it is difficult to recover

Method used

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  • A rocket fairing recovery system and method
  • A rocket fairing recovery system and method
  • A rocket fairing recovery system and method

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Embodiment Construction

[0033] 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 some 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.

[0034] In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer" etc. The indicated orientation or positional relationship 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 referred device or element must have a specific orientation, ...

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Abstract

The invention provides a rocket fairing recovery system and method, belonging to the technical field of rocket fairing recovery, wherein the rocket fairing recovery system includes: a guide structure, a traction device and a soft landing structure; the guide structure includes a Rudders and canards on the cover; the traction device includes an aircraft and a docking structure, the aircraft is connected with the fairing through the docking structure; the soft landing structure includes an air bag, the air bag is arranged on the fairing, and the air bag is inflated The back is positioned at the below of the fairing of flying posture; The recovery system of rocket fairing of the present invention adopts guide structure to control the flight track of fairing in high altitude, and adopts aircraft to tow fairing in low altitude, so that fairing To slide towards the designated landing area, the soft landing structure can make the fairing slide on land, and buffer the impact of the fairing, so that the fairing can be recovered smoothly, thereby reducing the difficulty of recovering the fairing.

Description

technical field [0001] The invention relates to the technical field of recovery of rocket fairings, in particular to a recovery system and method for rocket fairings. Background technique [0002] The rocket fairing is made of high-strength, lightweight, high-temperature-resistant, and radio-transparent materials. It is located on the top of the launch vehicle. While maintaining the aerodynamic shape of the rocket, it puts a solid armor on the payload spacecraft. [0003] Before the rocket takes off, the fairing protects the spacecraft on the ground to ensure the requirements of the spacecraft for temperature, humidity and cleanliness. When the rocket is lifted through the atmosphere, the fairing can protect the spacecraft from damage caused by aerodynamic force and aerodynamic heat. After the launch vehicle flies out of the atmosphere, the fairing will be divided into two halves along the longitudinal direction of the rocket body and thrown away to complete its mission and...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F42B15/00F42B15/01
CPCF42B15/00F42B15/01B64G1/002B64D5/00B64G1/62B64G1/2227
Inventor 彭小波郑立伟施发树
Owner BEIJING XINGJI RONGYAO SPACE TECH CO LTD