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GB/T 38924.3-2020Environmental test methods for civil small and light unmanned aircraft system—Part 3: High-temperature test (English PDF)

民用轻小型无人机系统环境试验方法 第3部分:高温试验

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Issued by

SAMR; SAC

Level / Type

National · Recommended

Issue date

July 21, 2020

Implementation date

February 1, 2021

Scope

GB/T 38924.3-2020 is the English-translated version of 民用轻小型无人机系统环境试验方法 第3部分:高温试验.

GB/T 38924.3-2020 is the Chinese standard "Environmental test methods for civil small and light unmanned aircraft system—Part 3: High-temperature test".

Its scope clause reads: This part of GB/T 38924 specifies the civil light and small UAV (take-off weight between 0.25kg and 150kg) system (including flying Test conditions, test equipment and instruments, test process, test interruption and recovery, test result evaluation and test report.

This section applies to civilian light and small UAV systems that may be affected by high temperature environments during use, so as to determine The ability of light and small UAV systems to withstand high temperature environments. Its clauses include terms and definitions; test conditions.

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Document preview — GB/T 38924.3-2020

National Standard of the People's Republic of China

ICS
49.020
Classification
V 35

Issued by: State Administration for Market Regulation; Standardization Administration of the PRC

Contents

  • 1 Scope1
  • 2 Normative references1
  • 3 Terms and definitions1
  • 4 Test conditions1
  • 4.1 High temperature storage test conditions1
  • 4.2 High temperature working test conditions2
  • 4.3 Device under test2
  • 5 Test equipment and instruments2
  • 6 Test process3
  • 6.1 High temperature storage test process3
  • 6.2 High temperature working test process3
  • 7 Test interruption and resumption4
  • 7.1 Under-test interruption4
  • 7.2 Test interruption4
  • 8 Evaluation of test results4
  • 8.1 High temperature storage test results4
  • 8.2 High temperature working test results4
  • 9 Test report5

1 Scope

This part of GB/T 38924 specifies the civil light and small UAV (take-off weight between 0.25kg and 150kg) system (including flying

Test conditions, test equipment and instruments, test process, test interruption and recovery, test result evaluation and test report.

This section applies to civilian light and small UAV systems that may be affected by high temperature environments during use, so as to determine

The ability of light and small UAV systems to withstand high temperature environments.

2 Normative references

The following documents are indispensable for the application of this document. For dated reference documents, only the dated version applies to this article

Pieces. For undated references, the latest version (including all amendments) applies to this document.

GB/T 38924.1-2020 Environmental test methods for civil light and small UAV systems Part 1.General

3 Terms and definitions

The following terms and definitions defined in GB/T 38924.1-2020 apply to this document.

3.1 High temperature storage temperature

During storage or exposure to climate extremes, the equipment is expected to be normally exposed to the highest ground temperature.

3.2 Operatinghightemperature

The highest temperature at which the equipment is normally exposed and required to work.

4 Test conditions

4.1 High temperature storage test conditions

4.1.1 Overview

Unless otherwise specified, the high temperature storage test shall be carried out in accordance with the following test conditions.

4.1.2 Test temperature

Determine the high temperature storage test temperature according to the relevant documents. If the relevant documents do not specify the high temperature storage test temperature, the recommended high temperature storage temperature is

70°C.

4.1.3 Test duration

Unless otherwise specified, the duration of the high temperature storage test is 3h after the equipment under test reaches a stable temperature.

......
This preview omits tables, figures, formulas and parts of the technical clauses. The complete document — 15 pages — is available in the English PDF.

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