BS EN 16603-70-41 addresses the utilization of telecommand packet and telemetry packets for the purpose of remote monitoring and control of space craft subsystems and payloads.
BS EN 16603-70-41 defines a set of services that satisfy all the fundamental operational requirements for spacecraft monitoring and control during spacecraft integration, testing and flight operations, refer to ECSS-E-ST-70-11. It also specifies the structure and contents of the telecommand packets used to transport the requests and the telemetry packets used to transport the reports.
BS EN 16603-70-41 can be used by any mission, no matter what its domain of application, orbit or ground station coverage characteristics. However, it is not the intention that the PUS should be applied in its entirety to a given mission.
The services defined in BS EN 16603-70-41 cover a wide spectrum of operational scenarios and, for a given mission, only a subset of these services is likely to be appropriate.
BS EN 16603-70-41 on telemetry and telecommand packet is applicable to:
Telemetry facilitates the transmission of space-acquired data from source to user in a standardised highly automated manner.
BS EN 16603-70-41 mainly addresses the requirements that apply to the spacecraft and its components.
BS EN 16603-70-41 provides guidelines on telemetry and telecommand packet that are used for transporting the request and reports with greater efficiency.
BS EN 16603-70-41:2017 supersedes EN 14776:2004. BS EN 16603-70-41:2017 includes some technical changes with respect to EN 14776:2004. These include:
EN 16603-70-41:2017