BackForwardInstrument:  TRSR 

Instrument details
Acronym TRSR
Full name Turbo Rogue Space Receiver
Purpose Precision orbitography
Short description Receiver for simultaneous acquisition of signals from a few satellites of the Global Positioning System (GPS)
Background Consolidated technology
Scanning Technique N/A
Resolution N/A
Coverage / Cycle N/A
Mass 10 kg Power 17.5 W Data Rate

 

Providing Agency NASA
Instrument Maturity Flown on operational programme
Utilization Period: 1998 to 2023
Last update: 2017-03-31
Detailed characteristics
Satellites this instrument is flying on

Note: a red tag indicates satellites no longer operational, a green tag indicates operational satellites, a blue tag indicates future satellites

Instrument classification
  • Other payload component
  • Positioning system
WIGOS Subcomponents No WIGOS subcomponents have been defined.
Mission objectives
Evaluation of Measurements

The following list indicates which measurements can typically be retrieved from this category of instrument. To see a full Gap Analysis by Variable, click on the respective variable.

Note: table can be sorted by clicking on the column headers
Note: * Primary mission objective.
VariableRelevance for measuring this variableOperational limitationsExplanation
Geoid4 - fairHighly indirect.Opportunity information from GNSS receiver used for precise orbit determination
Gravity field5 - marginalHighly indirect.Opportunity information from GNSS receiver used for precise orbit determination