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Rocket test parameter selection method and device, storage medium and electronic device

A technology of test parameters and storage medium, applied in the field of equipment environment engineering, can solve the problem that the adaptability of rocket flight environment cannot be fully verified, and achieve the effect of saving test resources and test time, reducing test cost, and satisfying environmental adaptability

Pending Publication Date: 2021-03-09
CHINA ACAD OF LAUNCH VEHICLE TECH
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Problems solved by technology

[0005] The embodiment of the present application provides a method for selecting rocket test parameters, a device, a storage medium, and an electronic device, so as to at least solve the problem that the adaptability of the rocket flight environment cannot be fully verified in related technologies

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  • Rocket test parameter selection method and device, storage medium and electronic device
  • Rocket test parameter selection method and device, storage medium and electronic device

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Embodiment Construction

[0021] In the process of realizing the present application, the inventor found that, for the whole arrow test, under the condition that the noise environment test conditions are well established, the noise test can assess the adaptability of the rocket body structure and the electrical equipment involved in the test to the noise environment. In recent years, studies have shown that the vibration during flight is mainly caused by flight noise. Therefore, when the boundary conditions are simulated sufficiently, the noise test can simultaneously verify the adaptability of the structure and the product to the flight vibration environment.

[0022] There are at least the following problems in the rocket noise environment test: 1. The size of the whole rocket is large, and the noise test of the whole rocket has a high demand for the test site and it is difficult to simulate the free boundary; The current cabin-level noise test cannot simulate the real boundary conditions; 3. Due to t...

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Abstract

The embodiment of the invention provides a rocket test parameter selection method and device, a storage medium and an electronic device. The method comprises the steps that one or more target cabins are selected from a rocket to be tested; determining a test condition for the target cabin section, the test condition comprising a noise environment test condition; and determining test equipment according to the noise environment test condition, the test equipment comprising equipment for noise test. By the adoption of the scheme, it is ensured that the environmental adaptability of the rocket meets the requirement, meanwhile, the test cost is reduced, and test resources and test time are saved.

Description

technical field [0001] This application relates to equipment environment engineering technology, in particular, to a method for selecting rocket test parameters, a device, a storage medium, and an electronic device. Background technique [0002] The noise test is an important large-scale ground environment test in the rocket development process. The noise test simulates the sound field during the flight and applies it to the tested product to verify the environmental adaptability of the product. [0003] For the whole arrow test, under the condition that the noise environment test conditions are fully established, the noise test can assess the adaptability of the rocket body structure and the electrical equipment involved in the test to the noise environment. However, due to the large size of the whole arrow, the noise test of the whole arrow has the problems of high demand for the test site and difficulty in simulating the free boundary. [0004] Aiming at the problem that...

Claims

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Application Information

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IPC IPC(8): G06F30/20F42B35/02G06F119/10
CPCG06F30/20F42B35/02G06F2119/10
Inventor 余慕春李炳蔚张子骏丁晨王尧孙静怡牛智玲刘博马靓洪东跑高峰龚旻徐子健南宫自军马晓东刘博龙颜峰
Owner CHINA ACAD OF LAUNCH VEHICLE TECH
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