| Standard ID | Contents [version] | USD | STEP2 | [PDF] delivered in | Standard Title (Description) | Status | PDF |
| GB/T 32454-2015 | English | 150 |
Add to Cart
|
0--9 seconds. Auto-delivery
|
Flight evaluation of launch vehicle
| Valid |
GB/T 32454-2015
|
PDF similar to GB/T 32454-2015
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.
|