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BS EN 16603-50:2022 – TC:2023 Edition

$280.87

Tracked Changes. Space engineering. Communications

Published By Publication Date Number of Pages
BSI 2023 152
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This Standard specifies the requirements for the development of the end­to­end data communications system for spacecraft. Specifically, this standard specifies: – The terminology to be used for space communication systems engineering. – The activities to be performed as part of the space communication system engineering process, in accordance with the ECSS-E-ST-10 standard. – Specific requirements on space communication systems in respect of functionality and performance. The communications links covered by this Standard are the space­to­ground and space­to­space links used during spacecraft operations, and the communications links to the spacecraft used during the assembly, integration and test, and operational phases. Spacecraft end­to­end communication systems comprise components in three distinct domains, namely the ground network, the space link, and the space network. This Standard covers the components of the space link and space network in detail. However, this Standard only covers those aspects of the ground network that are necessary for the provision of the end­to­end communication services. NOTE Other aspects of the ground network are covered in ECSS-E ST 70. This Standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S ST 00.

PDF Catalog

PDF Pages PDF Title
1 30470544
71 A-30424982
72 undefined
80 1 Scope
81 2 Normative references
82 3 Terms, definitions and abbreviated terms
3.1 Terms defined in other standards
3.2 Terms specific to the present standard
85 3.3 Abbreviated terms
87 4 Space communications engineering principles
4.1 Context
88 4.2 Overall space communication
93 4.3 Space communication domains
4.3.1 Overview
4.3.2 Space network
4.3.2.1 Overview
94 4.3.2.2 On-board network
4.3.2.3 Inter-spacecraft network
4.3.3 Space link
95 4.3.4 Ground network
96 4.4 Communications engineering process
4.4.1 Introduction
4.4.2 Communication engineering activities
4.4.2.1 Overview
4.4.2.2 Communications engineering management
4.4.2.3 Requirement engineering
97 4.4.2.4 Analysis
4.4.2.5 Design and configuration
4.4.2.6 Implementation
4.4.2.7 Verification
98 4.4.2.8 Operations
4.4.3 Process milestones
4.5 Relationship with other standards
99 4.6 <>
4.7 Spacecraft control considerations
100 5 Requirements
5.1 Introduction
5.2 Space communication system engineering process
5.2.1 Requirements engineering
5.2.1.1 Overview
5.2.1.2 Activities
101 5.2.1.3 Outputs
5.2.2 Analysis
5.2.2.1 Overview
5.2.2.2 Activities
5.2.2.3 Outputs
102 5.2.3 Design and configuration
5.2.3.1 Overview
5.2.3.2 Activities
5.2.3.3 Outputs
103 5.2.4 Implementation
5.2.4.1 Overview
5.2.4.2 Activities
5.2.4.3 Outputs
104 5.2.5 Verification
5.2.5.1 Overview
5.2.5.2 Activities
5.2.5.3 Outputs
105 5.2.6 Operations
5.2.6.1 Overview
5.2.6.2 Activities
5.2.6.3 Outputs
5.3 Space communication system
5.3.1 Bandwidth allocation
106 5.3.2 Congestion
5.3.3 Cessation of emission
5.4 Telecommanding
5.4.1 Commandability at all attitudes and rates
5.4.2 Telecommand delivery service
5.4.3 Erroneous telecommand rejection
5.4.4 Essential telecommand distribution
107 5.4.5 Command authentication
5.4.6 Command encryption
5.4.7 Commanding�in�the�blind
5.4.8 Telecommand acknowledgement
5.4.9 Hot redundancy of on-board telecommand chains
108 5.4.10 Telecommand destination identification
5.5 Telemetry
5.5.1 Telemetry at all attitudes and rates
5.5.2 Essential telemetry acquisition
109 5.5.3 Telemetry source identification
5.5.4 Telemetry�in�the�blind
5.5.5 Telemetry data time stamping
5.5.6 Simultaneous support of differing source rates
5.5.7 Telemetry authentication and encryption
110 5.6 Space link
5.6.1 Introduction
5.6.1.1 Overview
5.6.1.2 Conformity to ITU/RR
5.6.2 Directionality
5.6.3 Short contact periods
111 5.6.4 Interoperability
5.6.5 Orbits
5.6.6 Noise sources
5.6.7 Mission phases
5.6.8 Link setup times
5.6.9 Mixed isochronous and asynchronous traffic
112 5.6.10 Mixed housekeeping and payload data
5.6.11 Space link performance
5.6.11.1 Doppler shift and Doppler rate
5.6.11.2 Operation during tumbling
5.6.11.3 Tolerance of run lengths and transition densities
5.6.11.4 Failure modes
5.6.11.5 Uplink assumed bit error rate (BER)
5.6.11.6 Uplink frame rejection rate
113 5.6.11.7 Probability of accepting corrupted uplink frames
5.6.11.8 Downlink frame rejection rate
5.6.11.9 Probability of accepting corrupted downlink frames
5.6.11.10 Low delay
5.6.11.11 Downlink rates
5.6.12 Space link frequency
5.6.12.1 Space link media
114 5.6.12.2 Frequency band selection
5.6.12.3 Unwanted RF emissions
5.6.12.4 Power flux density limits
5.6.13 Space link protocol
5.6.13.1 Spacecraft and link identification
115 5.6.13.2 Data unit identifier
5.6.13.3 Sequence identifier
5.6.13.4 Error detection
5.6.13.5 ARQ settings
5.6.14 Space link service
5.6.14.1 Connection establishment and maintenance
116 5.6.14.2 Guaranteed delivery
5.6.14.3 Expedited delivery
5.6.14.4 Isochronous services
5.6.14.5 Isochronous requirements
5.6.14.6 Time correlation
117 5.6.14.7 Ranging and Doppler tracking
5.6.14.8 Telecommand receipt confirmation
5.6.14.9 Space link exception reporting
5.7 Space network
5.7.1 On-board network
5.7.1.1 Overview
5.7.1.2 Deterministic performance
118 5.7.1.3 Synchronous command and control
5.7.1.4 Asynchronous data transfers
5.7.1.5 On-board network medium access
5.7.1.6 Hot redundant operation of space network nodes
5.7.1.7 <>
5.7.1.8 On-board network error rates
5.7.2 On-board network services
5.7.2.1 Data transfer services
5.7.2.2 <>
5.7.2.3 Expedited transfer services
119 5.7.2.4 On-board network management service
5.7.2.5 On-board network redundancy management
5.7.2.6 On-board network exception reporting
5.7.2.7 Telecommand delivery confirmation
5.7.2.8 Time distribution
5.7.3 Inter-spacecraft network
5.7.3.1 Overview
5.7.3.2 Deterministic performance
120 5.7.3.3 Asynchronous data transfers
5.7.4 Inter-spacecraft network services
5.7.4.1 Data transfer services
5.7.4.2 Expedited transfer services
5.7.4.3 Inter-spacecraft network management service
5.7.4.4 Inter-spacecraft network exception reporting
5.7.4.5 Time synchronization
5.8 Ground network
5.8.1 Overview
121 5.8.2 Data labelling
5.8.3 Security
5.8.4 Error rates
5.8.5 Hot redundant operation of ground network nodes
5.8.6 Ground network availability
BS EN 16603-50:2022 - TC
$280.87