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GB/T 42044-2022: General design requirements for utilization payloads of space station
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GB/T 42044-2022: General design requirements for utilization payloads of space station

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General design requirements for utilization payloads of space station ICS 49.020 CCSV04 National Standards of People's Republic of China General design requirements for space station application payloads Published on 2022-10-12 2022-10-12 Implementation State Administration for Market Regulation Released by the National Standardization Administration directory Preface I 1 Scope 1 2 Normative references 1 3 Terms and Definitions 1 4 Payload classification 1 5 Design basis 2 6 Design Principles 2 7 Mechanical Design Requirements 2 8 Power supply design requirements 4 9 Thermal Design Requirements 6 10 Information and measurement and control design requirements 8 11 Design requirements for gas interface 9 12 Ergonomic Design Requirements 10 13 Medical Design Requirements 11 14 Security Design Requirements 12 15 Reliability Design Requirements 12 16 Maintainability Design Requirements 13 17 Testability Design Requirements 13 18 Electromagnetic Compatibility Design Requirements 13 19 Design Verification Requirements 14

foreword

This document is in accordance with the provisions of GB/T 1.1-2020 "Guidelines for Standardization Work Part 1.Structure and Drafting Rules of Standardization Documents" drafted. Please note that some content of this document may be patented. The issuing agency of this document assumes no responsibility for identifying patents. This document is under the jurisdiction of the National Standardization Technical Committee for Manned Spaceflight (SAC/TC570). This document is drafted by. Space Application Engineering and Technology Center, Chinese Academy of Sciences, Beijing Space Vehicle General Design Department, Chinese Astronaut Research and Training Center, Beijing Institute of Tracking and Communication Technology. The main drafters of this document. Liu Wei, Zhao Liping, Zhong Hongen, Zhang Lixian, Zhang Wei, Huang Kun, Liu Ying, Tao Xin, Yang Jinlu, Xu Wenlong, Fu Jun. General design requirements for space station application payloads

1 Scope

This document specifies the design basis, design principles, payload classification, general design and verification of payloads for space station applications certificate requirements. This document applies to the design and verification of payloads for applications inside and outside the space station cabin. Payload ascending with a cargo or manned spacecraft payload, the payload that goes down with the manned spacecraft, and the payload that carries out on-orbit actual (test) tests in cargo spacecraft, manned spacecraft and cargo airlocks The load can be used for reference.

2 Normative references

The contents of the following documents constitute essential provisions of this document through normative references in the text. Among them, dated citations documents, only the version corresponding to that date applies to this document; for undated references, the latest edition (including all amendments) applies to this document. GB/T 30114.1 Terminology of space science and its application part 1.basic general GB/T 34829 Space Station Application Payload Data Communication Specification GB/T 35439 Space Station Application Payload Safety, Reliability and Maintainability Guarantee General Requirements GB 50868 Construction Engineering Allowable Vibration Standard

3 Terms and Definitions

The terms and definitions defined in GB/T 30114.1 apply to this document.

4 Payload classification

The payloads are classified as follows. a) The load in the cabin mainly includes the standard load unit (SPU) of the experimental cabinet, the standard drawer unit (SDU) of the experimental cabinet, the independent load in the cabin, Standard unit load in the cabin, where. 1) SPU. It is fixedly installed in the scientific experiment cabinet in the cabin or the empty cabinet in the cabin by using the back plate, with standard interfaces and envelopes. An experimental device used to achieve specific scientific experimental goals. SPU standard envelope size can be 1x, 2x or 4x units; 2) SDU. It is installed in the scientific experiment cabinet in the cabin or the empty cabinet in the cabin with standard guide rails. It has standard interfaces and envelopes. An experimental device used to achieve specific scientific experimental goals. SDU standard envelope size can be 1x, 2x or 3x units; 3) Independent load in the cabin. installed in the sealed cabin of the space station, with independent and complete functions and performance, in addition to engine, electricity, heat, gas and other interfaces In addition to supporting scientific experiments and technical test loads that do not depend on other payloads to complete their tasks. In meeting the requirements of machine, electricity, heat, Under the constraints of gas and other interfaces, the independent load in the cabin can be individually designed; 4) Standard unit load in the cabin. the payload of the actual (test) test carried out in the standard unit in the cabin, its mechanical, power supply, information, heat Interfaces such as vacuuming and vacuuming are provided by the standard unit in the cabin. The standard unit load in the cabin is generally divided into four specifications, namely. Type I, Type II, Type III, Type IV. b) Outboard loads mainly include standard outboard loads and non-standard outboard loads. Among them, the standard outboard loads can be divided into medium-sized standard outboard loads. ...