|
China space standard system number
|
Standard number
|
Title
|
1
|
CNSA-MA000001
|
GB/T 29072-2012
|
Preparing principles of technical network for spacecraft development
|
2
|
CNSA-MA000002
|
GB/T 29073-2012
|
Preparing principles of schedule network for spacecraft development
|
3
|
CNSA-MC000001
|
GB/T 29083-2012
|
Safety requirements for flammable materials, explosive devices, toxic gas and radioactive sources in spacecraft
|
4
|
CNSA-QA000001
|
GB/T 29076-2012
|
Execution requirements for quality problem close loop of space product
|
5
|
CNSA-QCD00001
|
GB/T 29074-2012
|
Requirements for qualification of components for space application
|
6
|
CNSA-QEDCA001
|
QJ 20285-2014
|
Test method of atomic oxygen effect for spacecraft materials
|
7
|
CNSA-QEDCA002
|
QJ 20286-2014
|
Test method of solar ultraviolet radiation effect for space non-metallic materials
|
8
|
CNSA-E0000001
|
GB/T 29082-2012
|
Storage requirements for satellite
|
9
|
CNSA-EA000001
|
GB/T 29079-2012
|
Classification and parameter symbols for orbits and trajectories of spacecraft
|
10
|
CNSA-EA000002
|
GB/T 29078-2012
|
Design guidelines for spacecraft launch window
|
11
|
CNSA-EA000003
|
GB/T 29084-2012
|
Grounding requirements of spacecraft
|
12
|
CNSA-EA000004
|
QJ 20001-2011
|
Terminology for lunar exploration program
|
13
|
CNSA-EA000005
|
QJ 20002-2011
|
Lunar probe coordinate system
|
14
|
CNSA-EA000006
|
GB/T 29085-2012
|
Technical requirements of contamination control for satellite
|
15
|
CNSA-EE000001
|
GB/T 29077-2012
|
Launch-vehicle-to-spacecraft flight environments telemetry data processing requirement
|
16
|
CNSA-SAA00001
|
QJ 20094-2012
|
Terminology for ground processing system of land observation satellites
|
17
|
CNSA-SAA00002
|
QJ 20098-2012
|
Technical requirements for data products and information management of land observation satellites
|
18
|
CNSA-SBB00001
|
QJ 1955A-2011
|
Terminology for space environment of spacecraft
|
19
|
CNSA-SBBB0001
|
QJ 20125-2012
|
Process for determining solar irradiances
|
20
|
CNSA-SC000001
|
GB/T 29080-2012
|
Evaluation for flight results of geosynchronous communications satellite
|
21
|
CNSA-MB000010
|
GB/T 32308-2015
|
Requirements for post-mission disposal of GEO satellites
|
22
|
CNSA-MB000013
|
GB/T 32295-2015
|
Design requirements for residual propellant venting of launch vehicle
|
23
|
CNSA-QEDCA003
|
QJ 20289A-2016
|
Test method for total ionizing radiation effect of spacecraft non-metal materials
|
24
|
CNSA-QEDCA016
|
QJ 20288A-2016
|
Test method for particle and ultraviolet radiation combined effects of spacecraft thermal control materials
|
25
|
CNSA-QEDCA024
|
QJ 1371B-2016
|
Test method for volatile condensable materials in vacuum
|
26
|
CNSA-QEDCA025
|
QJ 1558B-2016
|
Test method for materials outgassing performance in vacuum
|
27
|
CNSA-EA000007
|
GB/T 32296-2015
|
General reference frames for launch vehicle and spacecraft
|
28
|
CNSA-EA000009
|
GB/T 32302-2015
|
Interface requirements for launch vehicle and spacecraft
|
29
|
CNSA-EA000014
|
GB/T 32298-2015
|
Matching test requirements for spacecraft and launch vehicle
|
30
|
CNSA-EA000021
|
GB/T 29081-2012
|
Spacecraft Modal Analysis
|
31
|
CNSA-EF000004
|
GB/T 32304-2015
|
Electrostatic discharge protection requirements for aerospace electronic products
|
32
|
CNSA-EGA00005
|
GB/T 32307-2015
|
Assessment and control methods of spacecraft magnetic property
|
33
|
CNSA-EGA00015
|
QJ 20422.1-2016
|
Environment test methods for spacecraft unit - Part 1: Surface charging and discharging test
|
34
|
CNSA-EGA00016
|
QJ 20422.2-2016
|
Environment test methods for spacecraft unit - Part 2: Atomic oxygen test
|
35
|
CNSA-EGA00017
|
QJ 20422.3-2016
|
Environment test methods for spacecraft unit - Part 3: Solar ultraviolet irradiation test
|
36
|
CNSA-EGA00018
|
QJ 20422.4-2016
|
Environment test methods for spacecraft unit - Part 4: Magnetic test
|
37
|
CNSA-EGA00019
|
QJ 20422.5-2016
|
Environment test methods for spacecraft unit - Part 5: Vacuum cold welding test
|
38
|
CNSA-EGA00020
|
QJ 20422.6-2016
|
Environment test methods for spacecraft unit - Part 6: Acceleration test
|
39
|
CNSA-EGA00021
|
QJ 20422.7-2016
|
Environment test methods for spacecraft unit - Part 7: Vibration test
|
40
|
CNSA-EGA00022
|
QJ 20422.8-2016
|
Environment test methods for spacecraft unit - Part 8: Acoustic test
|
41
|
CNSA-EGA00023
|
QJ 20422.9-2016
|
Environment test methods for spacecraft unit - Part 9:Shock test
|
42
|
CNSA-SAA00006
|
QJ 20095-2012
|
Criteria for construction and operation of ground processing system of land observation satellites
|
43
|
CNSA-SAA00045
|
QJ 20099.1A-2016
|
Assessment method for remote sensing image quality of land observation satellites - Part 1: Optical remote sensors
|
44
|
CNSA-SAA00046
|
QJ 20100.1A-2016
|
Regulations for radiometric and geometric in-orbit calibration of land observation satellites - Part 1: Optical remote sensors
|
45
|
CNSA-SD000002
|
GB/T 32454-2015
|
Flight analysis and evaluation of launch vehicle
|
46
|
CNSA-MB000006
|
QJ 20134A-2018
|
Risk assessment procedures for space debris impact to spacecraft
|
47
|
CNSA-MB000005
|
QJ 20128A-2018
|
Orbit lifetime estimation for space debris
|
48
|
CNSA-QEDCA023
|
QJ 1322A-2014
|
Test method for mass loss of materials in vacuum
|
49
|
CNSA-QEDCA006
|
QJ 20287-2014
|
Test method of atomic oxygen and ultraviolet radiation synergistic effects for spacecraft materials
|
50
|
CNSA-QEDCA004
|
QJ 20627-2016
|
Electron irradiation test method for spacecraft materials
|
51
|
CNSA-QEDCA005
|
QJ 20628-2016
|
Test method of combined radiation effects for spacecraft materials
|
52
|
CNSA-QEDCA007
|
QJ 20629-2016
|
Test method of atomic oxygen and thermal cycling combined simulated environments for spacecraft materials
|
53
|
CNSA-QEDCA008
|
QJ 20630-2016
|
Test method of atomic oxygen and charged particle combined simulated environments for spacecraft materials
|
54
|
CNSA-QDCA0002
|
QJ 326B-2018
|
Packaging and storage of fasteners
|
55
|
CNSA-EF000013
|
GB/T 6496-2017
|
Test methods of aerospace solar cells calibration
|
56
|
CNSA-EF000014
|
GB/T 6494-2017
|
Measurement methods for electrical characteristics of aerospace solar cells
|
57
|
CNSA-EGA00024
|
QJ 20678.1-2018
|
Development requirements for space environment simulator — Part 1: Vacuum test
|
58
|
CNSA-EGA00025
|
QJ 20678.2-2018
|
Development requirements for space environment simulator — Part 2: Cryogenic system
|
59
|
CNSA-EGA00026
|
QJ 20678.3-2018
|
Development requirements for space environment simulator — Part 3: Environmental heat flow simulation system
|
60
|
CNSA-EGA00027
|
QJ 20678.4-2018
|
Development requirements for space environment simulator — Part 4: Solar simulator
|
61
|
CNSA-EGA00028
|
QJ 20678.5-2018
|
Development requirements for space environmental simulator — Part 5: Control and monitoring system
|
62
|
CNSA-EGA00029
|
QJ 20678.6-2018
|
Development requirements for space environment simulator — Part 6: System test
|
63
|
CNSA-SAA00003
|
GB/T 34518-2017
|
Requirements of data transmission and exchange interface for land observation satellite ground system
|
64
|
CNSA-SAA00010
|
GB/T 34514-2017
|
Requirements of remote sensing data distribution and user service for land observation satellite
|
65
|
CNSA-SAA00010
|
QJ 20005A-2018
|
Product formats and requirements of land observation satellites data
|
66
|
CNSA-MB000014
|
GB/T 34523-2017
|
Estimating methods for the mass of remaining propellant of spacecraft
|
67
|
CNSA-QA000020
|
QJ 1717A-2001
|
Requirements for preparation of quality record sheets in production process
|
68
|
CNSA-QCB00003
|
QJ 10004A-2018
|
Total dose radiation testing method of semiconductor devices for space applications
|
69
|
CNSA-QCB00004
|
QJ 10005A-2018
|
Test guidelines of single event effects induced by heavy ions of semiconductor devices for space applications
|
70
|
CNSA-QDCB0005
|
QJ 20024-2011
|
Nuts test methods
|
71
|
CNSA-QDCB0006
|
QJ 20025A-2018
|
Bolts test methods
|
72
|
CNSA-QEDBA009
|
QJ 2305A-2018
|
Test method for tensile properties of carbon/carbon composite materials
|
73
|
CNSA-QEDBA010
|
QJ 971A-2011
|
Test method for tensile properties of small specimens of fiber-reinforced plastics
|
74
|
CNSA-QEDBB005
|
QJ 2508A-2018
|
Determination for cure reaction temperature and reaction heat of epoxy resins — Differential scanning calorimetry
|
75
|
CNSA-QEDCA019
|
GB/T 34517-2017
|
Evaluating method for spacecraft nonmetal materials outgassing in vacuum
|
76
|
CNSA-QEDCA020
|
QJ 20700-2018
|
Test method for radiation induced conductivity of dielectric materials in space
|
77
|
CNSA-QEDCA026
|
QJ 20701-2018
|
Test method for intrinsic conductivity of dielectric materials in space — Charge storage method
|
78
|
CNSA-QEDCA027
|
QJ 20702-2018
|
Test method for secondary electron emission coefficient of dielectric materials in space — Pulsed method
|
79
|
CNSA-QEDCA028
|
QJ 20703-2018
|
Test method for interior charging and discharging property parameter of dielectric materials in space
|
80
|
CNSA-QEDDH001
|
QJ 2859A-2018
|
Application method and decision rule of industrial endoscope operation
|
81
|
CNSA-QEDDG002
|
QJ 3089A-2018
|
Helium leak detection method by mass spectrometer
|
82
|
CNSA-QEDDG008
|
QJ 3253A-2018
|
Test methods for leak detection using bubble emission techniques
|
83
|
CNSA-QEDDG009
|
QJ 2053A-2018
|
General requirements and methods for leak detection of spacecraft
|
84
|
CNSA-EA000020
|
QJ 2258B-2018
|
Measure methods for mass properties of spacecraft
|
85
|
CNSA-EA000035
|
GB/T 32455-2015
|
Terminology of Launch Vehicle
|
86
|
CNSA-EA000036
|
GB/T 34512-2017
|
Requirement for interface of manned spacecraft peripheral docking mechanism
|
87
|
CNSA-EB000004
|
QJ 20714-2018
|
Spacecraft structural analysis guideline — Structure modeling and checkout
|
88
|
CNSA-EB000005
|
QJ 20715-2018
|
Spacecraft structural analysis guideline — Modal analysis
|
89
|
CNSA-EB000006
|
QJ 20716-2018
|
Spacecraft structural analysis guideline — Static analysis
|
90
|
CNSA-EB000007
|
QJ 20717-2018
|
Spacecraft structural analysis guideline — Sinusoidal vibration
|
91
|
CNSA-EF000002
|
QJ 2041A-2018
|
Terminology of aerospace batteries and special power-source
|
92
|
CNSA-EF000015
|
QJ 20688-2018
|
Test method for secondary arc of spacecraft high-voltage solar cell array
|
93
|
CNSA-EGA00011
|
GB/T 34515-2017
|
Thermal balance test method for spacecraft
|
94
|
CNSA-EGA00012
|
GB/T 34522-2017
|
Thermal Vacuum Test Method for Spacecraft
|
95
|
CNSA-EGA00013
|
GB/T 34516-2017
|
Vibration test method for spacecraft
|
96
|
CNSA-EGA00030
|
QJ 1846A-2018
|
Requirements for temperature measurement and data processing of spacecraft thermal test
|
97
|
CNSA-EGA00031
|
QJ 1939A-2018
|
Verification methods for main parameters of the space simulator
|
98
|
CNSA-SAA00008
|
QJ 20097-2012
|
Requirements for data and information security of ground processing system of land observation satellite
|
99
|
CNSA-SAA00028
|
GB/T 34509.1-2017
|
In-orbit field radiometric calibration for optical remote sensor of land observation satellite Part 1: Visible-near infrared
|
100
|
CNSA-SAA00029
|
GB/T 34509.2-2017
|
In-orbit field radiometric calibration for optical remote sensor of land observation satellite Part 2: Thermal infrared
|
101
|
CNSA-SAA00047
|
QJ 3266A-2018
|
Technical requirements for ground station of land observation satellite
|
102
|
CNSA-SAA00048
|
QJ 3150A-2018
|
Technical requirements for earth observation satellite to remote sensing ground station
|
103
|
CNSA-SAC00013
|
GB/T 34966.1-2017
|
Internet-based transmission of GNSS augmentation information Part 1: Broadcast architecture
|
104
|
CNSA-SAC00014
|
GB/T 34966.2-2017
|
Internet-based transmission of GNSS augmentation information Part 2: Interface requirements
|
105
|
CNSA-SAC00015
|
GB/T 34966.3-2017
|
Internet-based transmission of GNSS augmentation information Part 3: Data transmission format
|
106
|
CNSA-QA000008
|
QJ 20136-2012
|
Requirements for space product assurance management
|
107
|
CNSA-QEDCA021
|
QJ 20291-2014
|
Test method of the outgassing rate for cryogenic insulation paper
|
108
|
CNSA-QEDBE007
|
QJ 20408-2016
|
Test method for specific heat capacity of liquid at low temperature
|
109
|
CNSA-QEDCA018
|
QJ 20409-2016
|
Test method for charging and discharging property of spacecraft surface materials
|
110
|
CNSA-EGA00039
|
QJ 20540-2016
|
Safety requirements for mechanical test of spacecraft
|
111
|
CNSA-MC000002
|
GB/T 37833-2019
|
General requirements for safety protection of spacecraft
|
112
|
CNSA-MB000015
|
GB/T 38194-2019
|
Design requirements for mitigation of operational debris of launch vehicle
|
113
|
CNSA-EGA00014
|
GB/T 38201-2019
|
Performance test method for spacecraft under ambient pressure and thermal environment
|
114
|
CNSA-EF000016
|
GB/T 38190-2019
|
Test method of electron irradiation aerospace solar cells
|
115
|
CNSA-EF000018
|
GB/T 38200-2019
|
Measurement method for quantum efficiency of solar cells
|
116
|
CNSA-EGA00032
|
QJ 20017A-2019
|
Low pressure discharging and multipacting test method for spacecraft
|
117
|
CNSA-EA000013
|
QJ 20075A-2019
|
Compilation requirements for electrical test program of spacecraft
|
118
|
CNSA-EF000019
|
QJ 20325.1A-2019
|
Test method for spacecraft RF components and equipment — Part 1: Low pressure discharge
|
119
|
CNSA-EF000020
|
QJ 20325.2A-2019
|
Test method for spacecraft RF components and equipment — Part 2: Multipaction
|
120
|
CNSA-EF000021
|
QJ 20325.3A-2019
|
Test method for spacecraft RF components and equipment — Part 3: Power handling
|
121
|
CNSA-EF000022
|
QJ 20325.4A-2019
|
Test method for spacecraft RF components and equipment — Part 4: Passive intermodulation (PIM)
|
122
|
CNSA-EF000005
|
QJ 20515-2016
|
Test method for spacecraft low-frequency cable
|
123
|
CNSA-EB000010
|
QJ 20534.2-2016
|
Ground tests of lunar probe —Part 2:Test method for landing impact
|
124
|
CNSA-EB000011
|
QJ 20534.3-2016
|
Ground tests of lunar probe —Part 3:Test method for landing stability
|
125
|
CNSA-EB000012
|
QJ 20534.4-2016
|
Ground tests of lunar probe —Part 4:Test method for locomotion performances
|
126
|
CNSA-EB000013
|
QJ 20536-2016
|
Mechanism polarity rules for deep space probe
|
127
|
CNSA-EGA00033
|
QJ 20537.1-2016
|
Requirements and methods for field simulation of lunar environments-Part 1:Simulation of lunar soil
|
128
|
CNSA-EGA00034
|
QJ 20537.2-2016
|
Requirements and methods for field simulation of lunar environments-Part 2:Simulation of lunar topography
|
129
|
CNSA-EGA00035
|
QJ 20537.3-2016
|
Requirements and methods for field simulation of lunar environments—Part 3:Simulation of low gravity
|
130
|
CNSA-EGA00036
|
QJ 20537.4-2016
|
Requirements and methods for field simulation of lunar environments—Part4:Simulation of lunar dust
|
131
|
CNSA-EGA00037
|
QJ 20537.5-2016
|
Requirements and methods for field simulation of lunar environments—Part5:Simulation of lunar light
|
132
|
CNSA-EGA00038
|
QJ 20537.6-2016
|
Requirements and methods for field simulation of lunar environments—Part6:Simulation of ultra cryogenic temperature
|
133
|
CNSA-EB000014
|
QJ 20611-2016
|
Guide for landing gear design of lunar probe
|
134
|
CNSA-EB000015
|
QJ 20612-2016
|
Test requirement for landing gear of lunar probe
|
135
|
CNSA-EGC00005
|
QJ 20854.1-2018
|
System-level electromagnetic compatibility simulation and analysis for launch vehicle Part 1: General specification
|
136
|
CNSA-EGC00006
|
QJ 20854.2-2018
|
System-level electromagnetic compatibility simulation and analysis for launch vehicle Part 2: Simulation modeling and debugging for wireless system
|
137
|
CNSA-EGC00007
|
QJ 20854.3-2018
|
System-level electromagnetic compatibility simulation and analysis for launch vehicle Part 3: Simulation of electromagnetic field distribution for wireless system
|
138
|
CNSA-EGC00008
|
QJ 20854.4-2018
|
System-level electromagnetic compatibility simulation and analysis for launch vehicle Part 4: Simulation of isolation for wireless system
|
139
|
CNSA-EGC00009
|
QJ 20854.5-2018
|
System-level electromagnetic compatibility simulation and analysis for launch vehicle Part 5: Calculation for frequency interfere of wireless system
|
140
|
CNSA-EGC00010
|
QJ 20854.6-2018
|
System-level electromagnetic compatibility simulation and analysis for launch vehicle Part 6: Cable coupling simulation
|
141
|
CNSA-EGA00040
|
QJ 20903-2018
|
Pressure environment test method for spacecraft products
|
142
|
CNSA-EF000023
|
QJ 2450A-2014
|
Interface requirements for solar array of spacecraft
|
143
|
CNSA-EGA00041
|
QJ 2630.1B-2019
|
Space environment test methods for spacecraft units — Part 1:Thermal vacuum test
|
144
|
CNSA-EGA00042
|
QJ 2630.2A-2019
|
Space environment test methods for spacecraft units— Part 2:Thermal balance test
|
145
|
CNSA-EGA00043
|
QJ 2630.3B-2019
|
Space environment test methods for spacecraft units — Part 3:Low pressure discharging and multipacting tests
|
146
|
CNSA-SAA00044
|
GB/T 38199-2019
|
Evaluation methods for optical image compression quality of land observation satellites
|
147
|
CNSA-SAA00049
|
GB/T 38028-2019
|
Gradation standard for panchromatic data products of remote sensing satellites
|
148
|
CNSA-SAA00050
|
GB/T 38026-2019
|
Gradation standard for multispectral data products of remote sensing satellite
|
149
|
CNSA-SAA00051
|
GB/T 38025-2019
|
Interface specification for remote sensing satellite ground system
|
150
|
CNSA-SAA00052
|
QJ 20614-2016
|
In-orbit test method for image swath of land observation satellite
|
151
|
CNSA-SAA00038
|
GB/T 38236-2019
|
Radiometric calibration method for space-borne optical remote sensors in laboratory
|
152
|
CNSA-SAA00053
|
QJ 20615-2016
|
In-orbit test method for MTF and spatial resolution based on target and point resources of land observation satellite
|
153
|
CNSA-SAA00054
|
QJ 20616-2016
|
In-orbit test method for image internal geometric accuracy of land observation satellite
|
154
|
CNSA-SAA00055
|
QJ 20617-2016
|
In-orbit test method for image geolocation accuracy of land observation satellite
|
155
|
CNSA-SAA00056
|
QJ 20618-2016
|
In-orbit test method for track drift of land observation satellite
|
156
|
CNSA-SAA00057
|
QJ 20619-2016
|
In-orbit test method for radiometric characteristic of land observation satellite
|
157
|
CNSA-SAA00058
|
QJ 20620-2016
|
In-orbit test method for spectral characteristic of land observation satellite
|
158
|
CNSA-QA000039
|
QJ 20981-2021
|
Quality control requirements for satellite assembly, integration and test process
|
159
|
CNSA-QA000024
|
QJ 2850B-2021
|
Foreign object debris prevention and control in space products
|
160
|
CNSA-QB000018
|
QJ 20987-2021
|
Worst case circuit simulation analysis for space electronic products
|
161
|
CNSA-QCC00147
|
GB/T 41033-2021
|
Design requirements of radiation hardening for CMOS IC
|
162
|
CNSA-QCD00068
|
GB/T 41032-2021
|
General guidelines for construction analysis components for space applications
|
163
|
CNSA-QCD00068
|
GB/T 41032-2021
|
General guidelines for construction analysis components for space applications
|
164
|
CNSA-MA000033
|
GB/T 40518-2021
|
Guidelines of technology readiness assessment for space engineering
|
165
|
CNSA-MA000034
|
GB/T 40520-2021
|
Rules for the product maturity of space equipment
|
166
|
CNSA-MB000016
|
GB/T 40536-2021
|
Design requirements for residual propellant venting of spacecraft
|
167
|
CNSA-MC000026
|
QJ 21010-2021
|
General requirements for space digital workshop
|
168
|
CNSA-EA000069
|
QJ 20894-2018
|
Factory test methods for launch vehicle upper stage
|
169
|
CNSA-EA000070
|
QJ 20756-2018
|
Stiffness distribution methods for the combined assembly of spacecraft and upper stage in multi-spacecraft launches
|
170
|
CNSA-EA000071
|
QJ 20757-2018
|
Thermal design criteria for launch vehicle upper stage
|
171
|
CNSA-EB000040
|
QJ 20292-2014
|
Finite element model checking methods for structural dynamic characteristics of launch vehicle
|
172
|
CCNSA-EB000041
|
QJ 20293-2014
|
Finite element analysis methods for loads of launch vehicle
|
173
|
CNSA-EB000042
|
QJ 20294-2014
|
Finite element analysis methods for structural dynamic characteristics of launch vehicle
|
174
|
CNSA-EB000043
|
QJ 20295-2014
|
Finite element analysis methods for structural strength of launch vehicle
|
175
|
CNSA-EB000044
|
QJ 20296-2014
|
Patran/Nastran based checking methods on the finite element model for structural strength of launch vehicle
|
176
|
CNSA-EB000045
|
QJ 20297-2014
|
Patran/Nastran based finite element modeling methods for structural strength of launch vehicle
|
177
|
CNSA-EB000046
|
QJ 20298-2014
|
Abaqus based checking methods on the finite element model for structural strength of launch vehicle
|
178
|
CNSA-EB000047
|
QJ 20299-2014
|
Abaqus based finite element modeling methods for structural strength of launch vehicle
|
179
|
CNSA-EB000048
|
QJ 20901-2018
|
Requirements of static combined test for bundled launch vehicle
|
180
|
CCNSA-EB000049
|
QJ 20876-2018
|
General integration requirements for space pyrotechnic devices
|
181
|
CNSA-EB000050
|
QJ 20759-2018
|
Safety use and management requirements of space pressure equipment
|
182
|
CNSA-ED000019
|
GB/T 40700-2021
|
Design requirements for autonomous navigation system of upper stage
|
183
|
CNSA-EE000041
|
QJ 20978-2021
|
Requirements of data interface for data transmission system of remote sensing satellite
|
184
|
CNSA-EE000042
|
QJ 20771-2018
|
Design requirements for image measuring system of launch vehicle
|
185
|
CNSA-EE000043
|
QJ 20772-2018
|
Synthetic test methods for image measuring system of launch vehicle
|
186
|
CNSA-EF000030
|
QJ 3019A-2018
|
Design requirements for solar array-batteries power system of spacecraft
|
187
|
CNSA-SAB00012
|
GB/T 12639-2021
|
Methods of in-orbit testing for GEO communication satellite payload performance
|
188
|
CNSA-SBBB0022
|
GB/T 41459-2022
|
Space environment—Space total solar irradiance
|