The payload/orbiter functional command signal flow and telemetry signal flow are discussed. Functional descriptions of the various orbiter communication/avionic equipment involved in processing a command to a payload either from the ground through the orbiter by the payload specialist on the orbiter are included. Functional descriptions of the various orbiter communication/avionic equipment involved in processing telemetry data by the orbiter and transmitting the processed data to the ground are presented. The results of the attached payload/orbiter single processing and data handling system evaluation are described. The causes of the majority of attached payload/orbiter interface problems are delineated. A refined set of required flux density values for a detached payload to communicate with the orbiter is presented.
Shuttle/payload communications and data systems interface analysis
1980-12-31
Sonstige
Keine Angabe
Englisch
Shuttle/Typical Payload Interface Study
NTIS | 1972
|Shuttle payload S-band communications system
NTRS | 1985
|Shuttle Payload S-Band Communications Study
NTIS | 1979
|Shuttle/typical payload interface study
NTRS | 1972
|Shuttle payload S-band communications study
NTRS | 1979
|