Path: Home > GB/T > Page31 > GB/T 32527-2016

Price & Delivery

US$219.00 · In stock · Download in 9 seconds
GB/T 32527-2016: Design specification of space materials science experimental facility -- Multifunctional high temperature furnace
Delivery: 9 seconds. True-PDF full-copy in English & invoice will be downloaded + auto-delivered via email. See step-by-step procedure
Status: Valid

Std ID	Version	USD	Buy	Deliver [PDF] in	Title (Description)
GB/T 32527-2016	English	219	Add to Cart	3 days [Need to translate]	Design specification of space materials science experimental facility -- Multifunctional high temperature furnace

GB/T 32527-2016: Design specification of space materials science experimental facility -- Multifunctional high temperature furnace

---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.
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. ...