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| GB/T 32302-2015 | English | 150 |
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Interface requirements for launch vehicle and spacecraft
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GB/T 32302-2015
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Basic data | Standard ID | GB/T 32302-2015 (GB/T32302-2015) | | Description (Translated English) | Interface requirements for launch vehicle and spacecraft | | Sector / Industry | National Standard (Recommended) | | Classification of Chinese Standard | V70 | | Classification of International Standard | 49.020 | | Word Count Estimation | 15,157 | | 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 corresponding interface requirements, interface verification methods (including analysis and testing), and the requirements for the joint operation of the launch vehicle and the launch vehicle, between the launch vehicle and the launched spacecraft (hereinafter referred to as the Arrow). This International Standard is applicable to the determination, verification and inspection of the interface relationships between launch vehicles for various spacecraft. | GB/T 32302-2015: Interface requirements for launch vehicle and spacecraft---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.
Interface requirements for launch vehicle and spacecraft
ICS 49.020
V70
National Standards of People's Republic of China
Requirements for Launch Vehicle and Spacecraft Interface
2015-12-31 released
2016-07-01 implementation
General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China
China National Standardization Management Committee released
Foreword
This standard is drafted in accordance with the rules given in GB/T 1.1-2009.
This standard is proposed by China Aerospace Science and Technology Corporation.
This standard is nationalized by the National Aeronautical Technology and Its Application Standardization Technical Committee (SAC/TC425).
The drafting of this standard. Beijing Aerospace Systems Engineering Research Institute.
The main drafters of this standard. Luo Heng, Zheng Liwei, Li Dan, Hu Wei, Lei Kai, Zhang Yibo, Li Jun, Li Guoyi, Sun Mu, He Wei, Wu Yitian,
Liu Jian, Liu Bing, Wang Xu, Cheng Xin, Xu Shan Shu, Xie Xuan.
Requirements for Launch Vehicle and Spacecraft Interface
1 Scope
This standard specifies the interface requirements between the launch vehicle and the launched spacecraft (hereinafter referred to as the Arrow). The interface verification method (including
Analysis and testing), as well as launch field equipment arrow joint operation requirements.
This standard applies to the identification, verification and inspection of the interface relationship between the launch vehicle and the various spacecraft.
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.
GB/T 32455 Carrier Terminology
3 terms and definitions
GB/T 32455 Definitions and the following terms and definitions apply to this document.
3.1
Spacecraft bracket (spacecraft adapter) payloadadaptor
Connecting the structure of the spacecraft and launch vehicle and the Arrow Connection Unlocking Device.
4 abbreviations
The following abbreviations apply to this document.
CDR --- Critical Design Review (CriticalDesignReview)
EMC --- Electromagnetic Compatibility (ElectromagneticCompatibility)
EMI --- electromagnetic interference (ElectromagneticInterference)
EIRP --- Equivalent radiant power (EffectiveIsotropicRadiatedPower)
FMAR --- Final Task Analysis Review (FinalMissionAnalysisReview)
ICD --- interface control file (InterfaceControlDocument)
PDR --- Preliminary Design Review (PreliminaryDesignReview)
PMAR --- Preliminary Task Analysis Review (PreliminaryMissionAnalysisReview)
RF --- radio frequency (RadioFrequency)
5 General requirements
5.1 Documentation requirements
5.1.1 The spacecraft system generally provides the following requirements for the carrier rocket system as follows.
a) technical requirements for spacecraft on launch vehicles;
b) spacecraft load coupling model;
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