Parachuting type recovery method used for first-stage rocket body recovery

A recovery method and rocket body technology, applied to projectiles, self-propelled bombs, offensive equipment, etc., can solve problems such as high cost, low success rate, and poor stability, and achieve the effect of low cost, ensuring success and stability

Active Publication Date: 2020-06-16
BEIJING LANDSPACETECH CO LTD
View PDF6 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] Aiming at the above-mentioned technical problems in the related art, the present invention provides a parachute-type recovery method for recovering the first-stage rocket body. By adopting the parachute-type recovery method, the poor stability and high cost of the traditional rocket recovery method are solved. , low success rate and other issues, it can make the rocket recovery process more convenient to control, safe and reliable, save costs, and improve the success and stability of rocket body recovery

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Parachuting type recovery method used for first-stage rocket body recovery
  • Parachuting type recovery method used for first-stage rocket body recovery
  • Parachuting type recovery method used for first-stage rocket body recovery

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0034] The technical solutions of the present invention will be further described below in conjunction with the accompanying drawings and through specific implementation methods. Spatially relative terms such as "below", "beneath", "under", "lower", "above", "on", "higher", etc. are used to facilitate description to explain the relative The orientation of two elements means that these terms are intended to encompass different orientations of the device in addition to orientations other than those shown in the figures. In addition, for example, "one element is on / under another element" may mean that two elements are in direct contact, or that there are other elements between the two elements. In addition, terms such as "first", "second", etc. are also used to describe various elements, regions, sections, etc. and should not be taken as limitations. Similar terms refer to similar elements throughout the description.

[0035] see figure 1 , the embodiment of the present invent...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention provides a parachuting type recovery method used for first-stage rocket body recovery. The parachuting type recovery method comprises the following steps that after a first-stage rocketbody and a second-stage rocket body are separated, the first-stage rocket body is turned over to the state that a separation cabin section is located above a lower power cabin section; a parachuting structure arranged on the power cabin section of the first-stage rocket body is opened to decelerate the first-stage rocket body; the sliding direction of the first-stage rocket body is controlled, sothat the first-stage rocket body flies to the position above the landing area; and when the first-stage rocket body lands, an implantation leg device is inserted into the surface of the landing area,and a landing stability augmentation support is flatly laid and unfolded along the surface of the landing area, so that the first-stage rocket body lands stably and recovery is completed. According tothe parachuting type recovery method used for first-stage rocket body recovery, the first-stage rocket body is turned over to the state that the separation cabin section faces downwards after being separated, then the parachuting structure is opened for speed reduction, the landing posture and direction of the rocket body are adjusted in real time, when the rocket body lands, the implantation legdevice is inserted into the landing area, and meanwhile the landing stability augmentation support is flatly laid and unfolded along the surface of the landing area, and therefore the first-stage rocket body lands stably and recovery is completed.

Description

technical field [0001] The invention relates to the technical field of rocket recovery, in particular to a parachute recovery method for recovery of a first-stage rocket body. Background technique [0002] With the rapid development of the aerospace industry, various technologies related to rockets have also achieved rapid progress. At present, as the only vehicle for launching satellites into space, continuous reduction of rocket manufacturing and launch costs is the goal pursued by major commercial aerospace companies. [0003] Taking rocket recovery as an example, the current mainstream rocket body recovery method is mainly the reverse thrust landing method represented by American Space X and Blue Origin. That is, by adding landing legs to the rocket body, the engine at the bottom of the rocket body is ignited multiple times when it is close to the ground, and the thrust is changed by the engine, and the position of the rocket is adjusted to achieve landing and fixed-poi...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
IPC IPC(8): F42B15/36F42B15/01F42B10/58
CPCF42B15/36F42B15/01F42B10/58
Inventor 杨瑞康车莉娜韩建业沈函默
Owner BEIJING LANDSPACETECH CO LTD
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products