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GB/T 32527-2016: Design specification of space materials science experimental facility -- Multifunctional high temperature furnace
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Design specification of space materials science experimental facility -- Multifunctional high temperature furnace
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GB/T 32527-2016
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PDF similar to GB/T 32527-2016
Standard similar to GB/T 32527-2016 GB/T 36258 GB/T 45678 GB/T 43367 Basic data | Standard ID | GB/T 32527-2016 (GB/T32527-2016) | | Description (Translated English) | Design specification of space materials science experimental facility -- Multifunctional high temperature furnace | | Sector / Industry | National Standard (Recommended) | | Classification of Chinese Standard | V36 | | Classification of International Standard | 49.090 | | Word Count Estimation | 11,154 | | Date of Issue | 2016-02-24 | | Date of Implementation | 2016-09-01 | | Quoted Standard | GB 150.3; GB/T 28878.1; GJB 151; GJB 450; GJB 900; GJB 3590; GJB 4009; GJB 6765 | | Regulation (derived from) | National Standard Announcement No | | 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 prescribes the general principles, design flow, general structure design, movement structure design, thermal control design, vacuum design, control design and teleoperation design of the multifunctional high temperature furnace for space material science experiment (hereinafter referred to as "multifunctional high temperature furnace")., Software design, ergonomic design, reliability, security design and design verification requirements. This standard applies to spacecraft, space laboratories, space stations and other space flight platform used in the design of multi-functional high-temperature furnace. In the satellite and other flight platforms on the multi-functional high-temperature furnace design can also refer to this standard. | GB/T 32527-2016: Design specification of space materials science experimental facility -- Multifunctional high temperature furnace
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Design specification of space materials science experimental facility - Multifunctional high temperature furnace
ICS 49.090
V36
National Standards of People's Republic of China
Space material science experiment device
Code for design of multi - purpose high - temperature furnace
2016-02-24 released
2016-09-01 implementation
General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China
China National Standardization Management Committee released
Directory
Preface I
1 Scope 1
2 normative reference document 1
3 Terms and definitions 1
Design General
5 design flow 2
Design Requirements 3
6.1 Overall structure design 3
6.2 Design of sports institutions 3
6.3 thermal control design 3
6.4 Vacuum design 3
6.5 Control design 3
6.6 teleoperation design 4
Software Design 4
6.8 ergonomic design 4
6.9 Reliability Security Design 4
6.10 Design Verification 5
Appendix A (informative) Composition and function of multifunctional high temperature furnaces 6
Reference 7
Foreword
This standard is drafted in accordance with the rules given in GB/T 1.1-2009.
This standard is under the jurisdiction of the National Committee on Standardization of Space Science and Its Application (SAC/TC312).
The drafting of this standard. Shanghai Institute of Ceramics, Chinese Academy of Sciences, Chinese Academy of Sciences National Space Science Center, Lanzhou space technology
Institute of Research.
The main drafters of this standard. Wen Haiqin, Liu Yan, Ai Fei, Pan Xiuhong, Feng Chude, Gao Guozhong, Tang Meibo, Yu Qiang, Zhang Zhengjun.
Space material science experiment device
Code for design of multi - purpose high - temperature furnace
1 Scope
This standard specifies the general principle of design of multi-functional high-temperature furnace (hereinafter referred to as "multi-function high-temperature furnace") of space material science experiment device
Process and overall structural design, motion design, thermal control design, vacuum design, control design, teleoperation design, software design, man-machine
Efficient design, reliability design and design verification requirements.
This standard applies to the design of multifunctional high temperature furnaces used in spacecraft, space laboratory, space station and other space flight platforms. in
Satellite and other flight platforms on the multi-functional high-temperature furnace design can also refer to this standard.
2 normative reference documents
The following documents are indispensable for the application of this document. For dated references, only the dated edition applies to this article
Pieces. For undated references, the latest edition (including all modifications) applies to this document.
Pressure vessels - Part 3. Design
Specification for rotating parts of space science - Part 1. Design terminology GB/T 28878-1
GJB151 Military equipment and subsystems Electromagnetic emission and sensitivity requirements
GJB450 equipment reliability work general requirements
GJB900 system security general outline
GJB3590 Aerospace system Electromagnetic compatibility requirements
Technical Requirements of Aerospace System for Spacecraft Application System of GJB4009
Ergonomics Requirement and Evaluation Method of Aerospace System for Spacecraft Engineering Design
3 terms and definitions
The following terms and definitions apply to this document.
3.1
Multifunctional high temperature oven multifunctionalhightemperaturefurnace
In the space microgravity environment for more than 400 ℃ material samples experimental study, with multi-temperature zone, multi-temperature field mode device.
Note. The material used for the study object is represented by a "material sample". Multi-functional high-temperature furnace itself, structural materials, electrical materials or thermal control materials with "materials"
Said.
3.2
Sample unit sampleunit
A unit consisting of a material sample and a structure of a sample carrying, fixing or encapsulating a material.
3.3
Sample store samplestorehouse
The mechanical structure of the sample unit is stored and fixed.
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