GB/T 32454-2015 English PDF

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Basic data

Standard ID: GB/T 32454-2015 (GB/T32454-2015)
Description (Translated English): Flight evaluation of launch vehicle
Sector / Industry: National Standard (Recommended)
Classification of Chinese Standard: V70
Classification of International Standard: 49.020
Word Count Estimation: 11,199
Date of Issue: 2015-12-31
Date of Implementation: 2016-07-01
Quoted Standard: GB/T 32455-2015
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 for the assessment of the results of the launch vehicle, the analysis of the overall and sub-systems, and the reporting requirements for the assessment results. This standard applies to launch vehicle flight test and application launch results analysis.

GB/T 32454-2015: Flight evaluation of 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.
Flight evaluation of launch vehicle ICS 49.020 V70 National Standards of People's Republic of China Analysis and Evaluation of Flight Result of Launch Vehicle 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. Wei Yuanming, Qin Xudong, Lei Kai, Wu Yitian, Li Guoyou, Xie Xuan, Zhu Dongge, Li Chongyuan, Lu Kai, Wang Jinghua, Li Huangli, Xu Qinghong, Zhu Pingping, Pan Hui. Analysis and Evaluation of Flight Result of Launch Vehicle

1 Scope

This standard specifies the general requirements for the evaluation of the results of the launch vehicle, the analysis of the overall and sub-system analysis and the results of the assessment Claim. This standard applies to carrier rocket flight test and application launch results analysis.

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 , The latest version (including all amendments) applies to this document. GB/T 32455-2015 Carrier Terminology

3 terms and definitions

The following definitions and definitions as defined in GB/T 32455-2015 apply to this document. 3.1 Payload payload An aircraft carried by a launch vehicle into a predetermined orbit, including satellites, detectors, spacecraft, etc. 3.2 Launch vehicle overall systemengineeringoflaunchvehicle To carry out the top of the launch vehicle design unit or professional collectively. Generally include. track, guidance and precision analysis, attitude control overall, electrical total Body, structure of the overall, separation of the overall, pneumatic and thermal environment, mechanical environment, the overall power, the ground and so on. 3.3 Carrier rocket subsystem subsystemoflaunchvehicle Receiving the overall design requirements or mission bookings of the launch vehicle, carrying out the specific design and implementation of the carrier rockets in one aspect or professional Said. General include. control systems, measurement systems (including telemetry systems and outer ballistic survey and safety control systems), propellant utilization systems, arrows (Including engine systems and pressurized delivery systems), ground launch support systems, fault detection and processing systems, escape systems Unified. 3.4 Subst subste The carrier rocket completes the separate part of the separate working stage after being separated, typically in a multi-stage series rocket. 3.5 Debris debris Rocket wreck After the child is separated, it falls on the ground (water) part. ......

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