Aerospace vehicle mass estimation method
A technology of aerospace vehicles and aircraft, applied in the direction of instruments, geometric CAD, design optimization/simulation, etc., can solve problems such as long cycle, difficult to meet fast demonstration, difficult analysis, etc., and achieve the effect of increasing speed
Pending Publication Date: 2022-07-22
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
View PDF0 Cites 0 Cited by
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
The existing technology is difficult to analyze the factors affecting the take-off weight of a single-stage aerospace vehicle, and the cycle is relatively long, which is difficult to meet the needs of rapid demonstration
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 moreImage
Smart Image Click on the blue labels to locate them in the text.
Smart ImageViewing Examples
Examples
Experimental program
Comparison scheme
Effect test
Embodiment Construction
[0074] In order to make the implementation purpose, technical solutions and advantages of the present application clearer, the technical solutions in the embodiments of the present application will be described in more detail below with reference to the accompanying drawings in the embodiments of the present application. Throughout the drawings, the same or similar reference numbers refer to the same or similar elements or elements having the same or similar functions. The described embodiments are some, but not all, of the embodiments of the present application. The embodiments described below with reference to the accompanying drawings are exemplary, and are intended to be used to explain the present application, but should not be construed as a limitation to the present application. Based on the embodiments in this application, all other embodiments obtained by those of ordinary skill in the art without creative work fall within the protection scope of this application. Th...
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
Login to View More Abstract
The invention belongs to the field of overall design of single-stage injection aerospace vehicles, and particularly relates to an aerospace vehicle mass estimation method. Comprising the steps of 1, obtaining a general equation of an aircraft acceleration process; 2, constructing a mass ratio estimation model of a rocket propulsion mode according to the general equation of the aircraft acceleration process; 3, according to the general equation of the aircraft acceleration process and the mass ratio estimation model of the rocket propulsion mode, constructing a mass ratio estimation model of an air-breathing propulsion mode; and 4, constructing a mass estimation model of the single-stage injection aerospace vehicle according to the mass ratio estimation model of the rocket propulsion mode and the mass ratio estimation model of the air-breathing propulsion mode. According to the method, estimation of the total mass of the single-stage injection aerospace vehicle is completed, the dynamic mode conversion point, the aircraft structure mass fraction, the law between the injection load and the total mass of the aircraft can be rapidly obtained, and the convergence speed of the scheme is increased.
Description
technical field [0001] The present application belongs to the field of overall design of a single-stage orbital aerospace vehicle, and particularly relates to a method for estimating the mass of an aerospace vehicle. Background technique [0002] A single-stage orbital aerospace vehicle is a reusable space-to-earth shuttle vehicle used to deliver orbital loads into orbital space. At present, there is still a lack of research on conceptual design methods suitable for single-stage orbiting vehicles at home and abroad, let alone a realistic single-stage orbiting vehicle for reference. The research work on the single-stage orbiting aerospace vehicle scheme mainly focuses on the scale evaluation of the whole system and the selection of aerodynamic layout. In the aspect of aircraft quality assessment research, the research work that has been carried out is mainly divided into two categories: one is to obtain the relationship between the size and mass of the aircraft through the s...
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
Login to View More Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/15G06F30/20G06F119/14
CPCG06F30/15G06F30/20G06F2119/14
Inventor 姚彦龙刘书博郎魁军
Owner SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA