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;
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)
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;
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)
