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GB/T 40544-2021: Spacecraft interface requirements document for launch vehicle services
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| Standard ID | Contents [version] | USD | STEP2 | [PDF] delivered in | Standard Title (Description) | Status | PDF |
| GB/T 40544-2021 | English | 404 |
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Spacecraft interface requirements document for launch vehicle services
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GB/T 40544-2021
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Basic data | Standard ID | GB/T 40544-2021 (GB/T40544-2021) | | Description (Translated English) | Spacecraft interface requirements document for launch vehicle services | | Sector / Industry | National Standard (Recommended) | | Classification of Chinese Standard | V01 | | Word Count Estimation | 22,298 | | Issuing agency(ies) | State Administration for Market Regulation, China National Standardization Administration | GB/T 40544-2021: Spacecraft interface requirements document for launch vehicle services---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.
Spacecraft interface requirements document for launch vehicle services
ICS 49.140
V01
National Standards of People's Republic of China
Spacecraft requirements documents for launch service interface
(ISO 17401.2004,Spacesystems-Spacecraftinterface
Released on 2021-08-20
2022-03-01 implementation
State Administration of Market Supervision and Administration
Issued by the National Standardization Management Committee
Foreword
This standard was drafted in accordance with the rules given in GB/T 1.1-2009.
The translation method used in this standard is equivalent to ISO 17401.2004 "Space System Spacecraft Launch Service Interface Requirements Document".
This standard has made the following editorial changes.
---Change the standard name to "Spacecraft to Launch Service Interface Requirements Document".
This standard was proposed and managed by the National Aerospace Technology and Application Standardization Technical Committee (SAC/TC425).
Drafting organizations of this standard. China Aerospace Standardization Institute, Nan'an Zhongji Standardization Research Institute Co., Ltd., Zhongke Wisdom (Dongying) Section
Technology Innovation Development Co., Ltd., Xiamen Keli Electronics Co., Ltd.
The main drafters of this standard. Huo Yuqian, Lin Xiaoping, Ning Jing, Yin Guangchi.
Introduction
This standard is used to guide the preparation of the interface requirement file (IRD) for launch services. The purpose of this standard is to promote spacecraft and transportation
Technical exchanges between carrier rocket systems. This standard reduces unnecessary launch service requirements to reduce spacecraft contractors and spacecraft manufacturing
The cost of the supplier is minimized.
In some cases, in order to provide comprehensive information, drawings are clearly required. All projects have stipulated a clear international system of units. If not
Appropriate, can be adjusted to the corresponding ratio.
When necessary, the spacecraft party may add other requirements. Certain sections of the IRD may refer to specific circumstances that are not applicable to launch services.
However, in this case, tailoring can be carried out.
Spacecraft requirements documents for launch service interface
1 Scope
This standard specifies a general template for the spacecraft side to compile the launch service interface requirements document. The interface requirements document lists the spacecraft’s
The main technical requirements for the launch vehicle and launch site when submitting the launch service application.
The interface requirements documents include the introduction of spacecraft launch tasks, mechanical and electrical interfaces, and overall environmental requirements (mechanical, thermal, cleanliness, wireless
Electrical-electrical), spacecraft development and testing programs, as well as launch site facilities and support requirements.
This standard is applicable to all active launch vehicles and related launch sites.
A relatively independent interface requirement document is convenient for the carrier to choose.
The interface requirement documents defined by this standard include the basic SC input data and interface control required by the carrier to compile interface control documents.
The document is drafted in accordance with ISO 15863.
2 Terms, definitions and abbreviations
2.1 Terms and definitions
The following terms and definitions apply to this document.
2.1.1
Available space usablevolume
The space within the LV fairing or load-bearing structure that is allowed to be used by the payload, and the static envelope of the spacecraft must not exceed this space to ensure
There is no physical contact between the spacecraft and the launch vehicle in a dynamic environment.
2.1.2
Spacecraft adapter spacecraftadapter; SCadapter
The structure that connects the spacecraft and the launch vehicle, and the connection and separation device of the star and arrow.
Note. The spacecraft adapter is part of the launch vehicle.
2.2 Abbreviations
The following abbreviations apply to this document.
EIRP---Equivalent isotropic radiated power (equivalent isotropic radiated power)
EMC---electromagnetic compatibility (electromagneticcompatibility)
IRD---interface requirement document (interfacerequirementdocument)
LV---launch vehicle
RF---radiofrequency
SC---spacecraft
Y/N---whether to respond (yes/noresponse)
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