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Matching test requirements for spacecraft and launch vehicle
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GB/T 32298-2015
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Basic data | Standard ID | GB/T 32298-2015 (GB/T32298-2015) | | Description (Translated English) | Matching test requirements for spacecraft and launch vehicle | | Sector / Industry | National Standard (Recommended) | | Classification of Chinese Standard | V70 | | Classification of International Standard | 49.020 | | Word Count Estimation | 11,126 | | Date of Issue | 2015-12-31 | | Date of Implementation | 2016-07-01 | | Quoted Standard | GB/T 32455 | | Regulation (derived from) | State Standard Announcement 2015 No.43 | | Issuing agency(ies) | General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China, Standardization Administration of the People's Republic of China | | Summary | This standard specifies the general requirements of the spacecraft and launch vehicle matching test, test objectives, test technology status, test content, test results analysis and summary. This standard applies to spacecraft and transport rocket between the matching test. | GB/T 32298-2015: Matching test requirements for spacecraft and launch vehicle---This is a DRAFT version for illustration, not a final translation. Full copy of true-PDF in English version (including equations, symbols, images, flow-chart, tables, and figures etc.) will be manually/carefully translated upon your order.
Matching test requirements for spacecraft and launch vehicle
ICS 49.020
V70
National Standards of People's Republic of China
The spacecraft and launch vehicle matching test requirements
Issued on. 2015-12-31
2016-07-01 implementation
Administration of Quality Supervision, Inspection and Quarantine of People's Republic of China
Standardization Administration of China released
Foreword
This standard was drafted in accordance with GB/T 1.1-2009 given rules.
The standard proposed by China Aerospace Science and Technology Corporation.
This standard by the National Aerospace Technology and Application of Standardization Technical Committee (SAC/TC425) centralized.
This standard was drafted. Beijing Aerospace System Engineering Institute.
The main drafters of this standard. LIU Bing, Mu Yu, Zhang Yi Park, Wang Jinghua, Wang Haitao, PROJECTILES, Liu, Li love, He Wei, Xie Xuan.
Introduction
Spacecraft and launch vehicle development process, the need for both sides of the interface and features to match the tests to verify spacecraft and launch vehicles
Mechanical interface, electrical interface, electromagnetic compatibility characteristics and whether the coordination between the arrows match. Matching mechanical interface, electrical interface, electromagnetic compatibility characteristics
Testing, spacecraft and launch vehicle is developed during routine testing of spacecraft and launch vehicles is a must attend the trial,
This standard conducted a more detailed description.
About vibration, modal noise, thermal environment interface test match should be based on the need to develop the spacecraft and launch vehicle, spacecraft analysis
And rocket assembly is subjected vibration, modal, noise, thermal environmental conditions, namely the development of environmental conditions for testing of spacecraft and launch vehicles
Indicators and carry out vibration respectively spacecraft and launch vehicles, modal noise, thermal environment tests, which are not the spacecraft and launch vehicle
Products must also participate in the test. The standard for a detailed statement of the test match each spacecraft and launch vehicle carried out jointly,
Does not involve vibration, modal test requirements match the noise, thermal environment interface.
To ensure the mechanical interface, electrical interface, electromagnetic compatibility characteristics of correctness, avoid combination of rocket and spacecraft in flight by a
Both interfaces and features that do not match the failure of development and testing tasks in aerospace engineering, the formation of spacecraft and launch vehicles match
Test guidelines and requirements. On this basis, further summarized by the formation of this standard to guide spacecraft and launch vehicle test match
Organization and implementation.
The spacecraft and launch vehicle matching test requirements
1 Scope
This standard specifies the general requirements for the spacecraft and launch vehicles (hereinafter referred to as the control arrows) match test, the test object, the test state of the art,
Test content, test result analysis and summary.
This standard applies to Test match between the spacecraft and the launch vehicle.
2 Normative references
The following documents for the application of this document is essential. For dated references, only the dated version suitable for use herein
Member. For undated references, the latest edition (including any amendments) applies to this document.
GB/T 32455 rocket term
3 Terms and Definitions
GB/T 32455 and defined by the following terms and definitions apply to this document.
3.1
Arrow Test match is matchingtestforspacecraftandlaunchvehicle
Verify that the interface between the spacecraft and launch vehicle correctness, coordination tests.
4 General requirements
4.1 Test Range
Arrow is matching tests include. Mechanical interface matching test, the electrical interface matching and electromagnetic compatibility test, is docked at the launch site arrow
test.
4.2 Test requirements for technical documentation
Arrow matching device testing process generally requires the use of the technical documentation for the following.
a) is state of the art Arrow test match should be consistent with the Interface Control Document spacecraft launch vehicle requirements;
b) state of the art control arrows shall meet the requirements of their respective special technical conditions; in meeting the matching test of the validity of the premise, can involve
Devices and components Bolt interface (system components) instead of the entire device, the entire arrow experiment, but its features and interfaces and models should be dedicated relationship skills
State operation conditions required consistency;
c) before the arrow matching test unit testing program should be prepared in accordance with this standard, and carry out control tests in accordance with the arrow matching test program and test processes.
4.3 test site, the environment and equipment requirements
Arrow to control test match venue, the environment and equipment general requirements are as follows.
a) test site, test environment should meet the emission simulator arrow assembly and flight status;
b) The test area shall meet the filter arrow match test products transportation, handling and testing requirements;
c) the test environment should meet the filter arrow on the temperature, humidity and cleanliness and other requirements;
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