Codeofchina.com is in charge of this English translation. In case of any doubt about the English translation, the Chinese original shall be considered authoritative.
Annex A to this standard is informative.
This standard was proposed by the Headquarters of the General Armaments Department of the PLA.
Interface requirement between launch site system and satellite system
1 Scope
This standard specifies the mission interface, general requirements, C3I interface and service support between aerospace launch site (hereinafter referred to as launch site) system and satellite system as well as basic process flow of satellite at launch site.
This standard is applicable to interface control between satellite and launch site, as well as technical preparation, service support and launch of satellite at launch site.
2 Normative references
The following normative documents contain provisions which, through reference in this text, constitute provisions of this standard. For dated references, subsequent amendments (excluding corrections) to, or revisions, of any of these publications do not apply. However parties to agreements based on this standard are encouraged to investigate the possibility of applying the most recent editions of the normative documents indicated below. For undated references or references with version not indicated, the latest edition of the normative document referred to applies.
GB 50057 Design code for protection of structures against lightning
GBJ 22 Specifications for the design of factory and mine roads
GJB 98 Anhydrous hydrazine
GJB 151 Electromagnetic emission and sensitivity requirements for military equipment and subsystems
GJB 753 Uns-dimethyl hydrazine
GJB 1673 Specification for nitrogen tetroxide
GJB 1696 Electromagnetic compatibility and grounding requirements of space system facilities
GJB 1963 Specification for methylhydrazine
GJB 2043 Environmental rule for aerospace launch site
GJB 2216 Requirements of package, storage and transportation for hydrazine fuels and nitro-oxidizers
3 Terms and definitions
For the purpose of this standard, the following term and definition apply.
basic process flow
main work flow for testing and launching satellites at launch site, including main work items and their priority, logistics direction and key technical status, implementation site and macro schedule of the main work items, etc.
4 Mission interface
4.1 Missions and requirements of launch site system
The missions and requirements of launch site system generally include:
a) review for the preparation of launch site system before satellite approach;
b) organization, command and coordination of launch missions, and formulation of general test documents such as “launch process flow in flight test ", "network diagram of test mission organization and implementation plan" and “collaborative command procedure for satellite-launch vehicle-ground integrated test";
c) lead role in organizing the quality and safety control of the launch mission, and security guard of the test site;
d) completion of or assistance in unloading, transporting, transferring, lifting and docking of products and equipment, and withdrawing from the site;
e) send of test information such as time, meteorology and progress of work to the satellite system;
f) provision of fixed infrastructure required for technical preparations and launch of the satellite;
g) provision of water, heating, electricity, gas, grounding and other support required for satellite launch test, and monitoring and management of electromagnetic environment of the launch site;
h) provision of technical service support for communication, meteorology, metrology, geodesy and special gas;
i) assistance in ensuring living guarantee of the test team during the mission.
4.2 Missions and requirements of satellite system
The missions and requirements of satellite system generally include:
a) ex-factory review of satellite and test equipment before entering the site;
b) organization, command and implementation of various tests for the system based on the overall test plan;
c) provision of relevant technical data to the launch site system, and submission of the zeroing report and quality report of each stage;
d) provision of relevant information needed for the organization, command and decision-making of the launch test to the launch site system.
4.3 Organization
In order to ensure the unified and smooth command and decision-making of launch missions, the organizations jointly established by the launch site system, satellite system and other test systems are as follows:
a) mission headquarters in launch site area: responsible for organizing and implementing the missions in launch site area, deploying the test plan, and making decisions to deal with major problems in the process of mission implementation;
b) quality control team: responsible for quality and safety control in the test process, coordinating, researching and dealing with major cross-system technical problems;
c) test and launch coordination team: responsible for work arrangement, plan coordination, operation control, technical problem handling and test site management during product test and launch, studying and formulating technical schemes, and coordinating and handling general technical problems;
d) technical safety team: responsible for all technical safety during the test of the test and launch system, inspecting, guiding and supervising the technical safety work of each test and launch system;
e) electromagnetic compatibility team: responsible for monitoring electromagnetic environment, controlling electromagnetic frequency and coordinating electromagnetic compatibility problems;
f) TT&C and communication technology coordination team: responsible for technical management, technical coordination, technical safety and quality control of TT&C and communication system, studying and formulating technical schemes to solve technical problems.
5 General requirements
5.1 Workshop configuration
5.1.1 Satellite final assembly test plant
Transfer room, final assembly test hall, system test room, unit test room, gas distribution room, product storage room, auxiliary room, etc. are configured.
5.1.2 Satellite filling and fairing assembly plant
Transfer room, filling hall, fairing assembly hall, gas distribution room, filling equipment room, auxiliary room, etc. are configured.
5.1.3 Test and launch control building
Test and launch command and control hall, test room, workshop, auxiliary room, etc. are configured.
5.1.4 Initiating explosive device room
Initiating explosive device storage room and test room are configured.
5.1.5 Launch station
Front-end equipment room, power supply room, tower workshop, satellite working platform of umbilical and service towers, air shower, passageway, etc. are configured.
5.2 Power supply and distribution
General requirements for power supply and distribution system in launch site are:
a) the power for satellite test and fire fighting is of the first class load, the power for satellite assembly, test and lighting is of the second class load, and the power for test shall be separated from that for working;
b) uninterruptible power supply (UPS) shall be arranged in important test places to supply power to process loads that are not allowed to be cut off instantaneously; satellite systems may also be provided with UPS power supply if necessary;
c) TN-C-S (three-phase five-wire system) is adopted for the power distribution system, and the type, quality and power of power supply shall meet the requirements of satellite test.
Foreword i 1 Scope 2 Normative references 3 Terms and definitions 4 Mission interface 4.1 Missions and requirements of launch site system 4.2 Missions and requirements of satellite system 4.3 Organization 5 General requirements 5.1 Workshop configuration 5.2 Power supply and distribution 5.3 Lightning protection and grounding 5.4 Electromagnetic compatibility 5.5 Environmental requirements 5.6 Water supply, drainage and fire fighting 5.7 Transportation 6 C3I interface between satellite and launch site 6.1 Interface 6.2 Information from C3I system to satellite network 6.3 Information from satellite network to C3I system 7 Service support 7.1 Communication 7.2 Special gas 7.3 Meteorology 7.4 Metrology 7.5 Geodesy 7.6 Hazard source 7.7 Other supports 7.8 Leaving equipment at site 7.9 Logistics support 8 Basic process flow 8.1 General requirements 8.2 Basic process flow chart of satellite 8.3 Main work contents of basic process flow Annex A (Informative) Main work in each stage of basic process flow A.1 Ground equipment unloading and transportation (A1) A.2 Ground equipment deployment and debugging (A2) A.3 Satellite unloading, transportation, transferring and in-place checking (M1) A.4 Unit testing (M2) A.5 Satellite assembly (M3) A.6 Satellite leak detection (M4) A.7 Whole-satellite electrical test (M5) A.8 Solar wing installation and test (M6) A.9 Filling preparation (M7) A.10 Satellite filling (M8) A.11 Satellite fairing installation (M9) A.12 Satellite transition and satellite-launch vehicle docking (M10) A.13 Satellite electrical test (M11) A.14 Satellite-launch vehicle joint checking (M12) A.15 Satellite operation before launch vehicle filling (M13) A.16 Near-launch checking (M14) A.17 Launch and flight state monitoring (M15) A.18 State recovery and withdrawal from the site (A3)
Codeofchina.com is in charge of this English translation. In case of any doubt about the English translation, the Chinese original shall be considered authoritative.
Annex A to this standard is informative.
This standard was proposed by the Headquarters of the General Armaments Department of the PLA.
Interface requirement between launch site system and satellite system
1 Scope
This standard specifies the mission interface, general requirements, C3I interface and service support between aerospace launch site (hereinafter referred to as launch site) system and satellite system as well as basic process flow of satellite at launch site.
This standard is applicable to interface control between satellite and launch site, as well as technical preparation, service support and launch of satellite at launch site.
2 Normative references
The following normative documents contain provisions which, through reference in this text, constitute provisions of this standard. For dated references, subsequent amendments (excluding corrections) to, or revisions, of any of these publications do not apply. However parties to agreements based on this standard are encouraged to investigate the possibility of applying the most recent editions of the normative documents indicated below. For undated references or references with version not indicated, the latest edition of the normative document referred to applies.
GB 50057 Design code for protection of structures against lightning
GBJ 22 Specifications for the design of factory and mine roads
GJB 98 Anhydrous hydrazine
GJB 151 Electromagnetic emission and sensitivity requirements for military equipment and subsystems
GJB 753 Uns-dimethyl hydrazine
GJB 1673 Specification for nitrogen tetroxide
GJB 1696 Electromagnetic compatibility and grounding requirements of space system facilities
GJB 1963 Specification for methylhydrazine
GJB 2043 Environmental rule for aerospace launch site
GJB 2216 Requirements of package, storage and transportation for hydrazine fuels and nitro-oxidizers
3 Terms and definitions
For the purpose of this standard, the following term and definition apply.
basic process flow
main work flow for testing and launching satellites at launch site, including main work items and their priority, logistics direction and key technical status, implementation site and macro schedule of the main work items, etc.
4 Mission interface
4.1 Missions and requirements of launch site system
The missions and requirements of launch site system generally include:
a) review for the preparation of launch site system before satellite approach;
b) organization, command and coordination of launch missions, and formulation of general test documents such as “launch process flow in flight test ", "network diagram of test mission organization and implementation plan" and “collaborative command procedure for satellite-launch vehicle-ground integrated test";
c) lead role in organizing the quality and safety control of the launch mission, and security guard of the test site;
d) completion of or assistance in unloading, transporting, transferring, lifting and docking of products and equipment, and withdrawing from the site;
e) send of test information such as time, meteorology and progress of work to the satellite system;
f) provision of fixed infrastructure required for technical preparations and launch of the satellite;
g) provision of water, heating, electricity, gas, grounding and other support required for satellite launch test, and monitoring and management of electromagnetic environment of the launch site;
h) provision of technical service support for communication, meteorology, metrology, geodesy and special gas;
i) assistance in ensuring living guarantee of the test team during the mission.
4.2 Missions and requirements of satellite system
The missions and requirements of satellite system generally include:
a) ex-factory review of satellite and test equipment before entering the site;
b) organization, command and implementation of various tests for the system based on the overall test plan;
c) provision of relevant technical data to the launch site system, and submission of the zeroing report and quality report of each stage;
d) provision of relevant information needed for the organization, command and decision-making of the launch test to the launch site system.
4.3 Organization
In order to ensure the unified and smooth command and decision-making of launch missions, the organizations jointly established by the launch site system, satellite system and other test systems are as follows:
a) mission headquarters in launch site area: responsible for organizing and implementing the missions in launch site area, deploying the test plan, and making decisions to deal with major problems in the process of mission implementation;
b) quality control team: responsible for quality and safety control in the test process, coordinating, researching and dealing with major cross-system technical problems;
c) test and launch coordination team: responsible for work arrangement, plan coordination, operation control, technical problem handling and test site management during product test and launch, studying and formulating technical schemes, and coordinating and handling general technical problems;
d) technical safety team: responsible for all technical safety during the test of the test and launch system, inspecting, guiding and supervising the technical safety work of each test and launch system;
e) electromagnetic compatibility team: responsible for monitoring electromagnetic environment, controlling electromagnetic frequency and coordinating electromagnetic compatibility problems;
f) TT&C and communication technology coordination team: responsible for technical management, technical coordination, technical safety and quality control of TT&C and communication system, studying and formulating technical schemes to solve technical problems.
5 General requirements
5.1 Workshop configuration
5.1.1 Satellite final assembly test plant
Transfer room, final assembly test hall, system test room, unit test room, gas distribution room, product storage room, auxiliary room, etc. are configured.
5.1.2 Satellite filling and fairing assembly plant
Transfer room, filling hall, fairing assembly hall, gas distribution room, filling equipment room, auxiliary room, etc. are configured.
5.1.3 Test and launch control building
Test and launch command and control hall, test room, workshop, auxiliary room, etc. are configured.
5.1.4 Initiating explosive device room
Initiating explosive device storage room and test room are configured.
5.1.5 Launch station
Front-end equipment room, power supply room, tower workshop, satellite working platform of umbilical and service towers, air shower, passageway, etc. are configured.
5.2 Power supply and distribution
General requirements for power supply and distribution system in launch site are:
a) the power for satellite test and fire fighting is of the first class load, the power for satellite assembly, test and lighting is of the second class load, and the power for test shall be separated from that for working;
b) uninterruptible power supply (UPS) shall be arranged in important test places to supply power to process loads that are not allowed to be cut off instantaneously; satellite systems may also be provided with UPS power supply if necessary;
c) TN-C-S (three-phase five-wire system) is adopted for the power distribution system, and the type, quality and power of power supply shall meet the requirements of satellite test.
Contents of GJB 7061-2010
Foreword i
1 Scope
2 Normative references
3 Terms and definitions
4 Mission interface
4.1 Missions and requirements of launch site system
4.2 Missions and requirements of satellite system
4.3 Organization
5 General requirements
5.1 Workshop configuration
5.2 Power supply and distribution
5.3 Lightning protection and grounding
5.4 Electromagnetic compatibility
5.5 Environmental requirements
5.6 Water supply, drainage and fire fighting
5.7 Transportation
6 C3I interface between satellite and launch site
6.1 Interface
6.2 Information from C3I system to satellite network
6.3 Information from satellite network to C3I system
7 Service support
7.1 Communication
7.2 Special gas
7.3 Meteorology
7.4 Metrology
7.5 Geodesy
7.6 Hazard source
7.7 Other supports
7.8 Leaving equipment at site
7.9 Logistics support
8 Basic process flow
8.1 General requirements
8.2 Basic process flow chart of satellite
8.3 Main work contents of basic process flow
Annex A (Informative) Main work in each stage of basic process flow
A.1 Ground equipment unloading and transportation (A1)
A.2 Ground equipment deployment and debugging (A2)
A.3 Satellite unloading, transportation, transferring and in-place checking (M1)
A.4 Unit testing (M2)
A.5 Satellite assembly (M3)
A.6 Satellite leak detection (M4)
A.7 Whole-satellite electrical test (M5)
A.8 Solar wing installation and test (M6)
A.9 Filling preparation (M7)
A.10 Satellite filling (M8)
A.11 Satellite fairing installation (M9)
A.12 Satellite transition and satellite-launch vehicle docking (M10)
A.13 Satellite electrical test (M11)
A.14 Satellite-launch vehicle joint checking (M12)
A.15 Satellite operation before launch vehicle filling (M13)
A.16 Near-launch checking (M14)
A.17 Launch and flight state monitoring (M15)
A.18 State recovery and withdrawal from the site (A3)
