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miniSLR® - Compact Satellite Laser Ranging System



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  • miniSLR prototype
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    The miniSLR prototype (version 1, October 2019) on the roof of the Institute of Technical Physics in Stuttgart. The whole system is integrated into a single housing and can easily be transported to another location.

    Credit: DLR (CC BY-NC-ND 3.0).

  • Laser Ranging
    Laser Ranging
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    In Satellite Laser Ranging (SLR) short laser pulses are emitted towards a satellite in orbit. On the satellite, a retroreflector bounces the light back towards the ground station. By measuring the light round trip time, the distance between ground station and satellite can be determined with high precision.

    Credit: DLR (CC BY-NC-ND 3.0).

  • Sample measurement
    Sample measurement
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    A laser ranging measurement of satellite Lageos-1 by the miniSLR. On the right y-axis, the measured distance is shown relative to the expected range. Averaged values (“normal points”) are indicated by red crosses. During this measurement the satellite is about 7,000 km away from the ground station.

    Credit: DLR (CC BY-NC-ND 3.0).

The miniSLR® system can be used to obtain millimetre-precise position data from satellites. These data have numerous applications in geodesy, Earth observation, satellite operation or to monitor decommissioned satellites. All that is required on the satellite is a lightweight and passive retro-reflector.

The miniSLR® can be integrated and tested at the factory before being deployed at its operation site. Thus, the full power of SLR becomes available at a fraction of the cost, development time, and on-site man-power when compared to traditional SLR set-ups. Its fully automatic operation reduces the running costs considerably.

As such, Satellite Laser Ranging becomes available or economically viable for new use cases and customers, such as operators of satellite navigation systems or geodetic institutes in the Global South. In addition, it can pave the way for new fields of application, such as monitoring satellite (mega-)constellations for high-precision orbit prediction and collision avoidance (Space Traffic Management, STM)

Technical specifications

Measurement Range  400 to 25 000 km
Accuracy (Normal Point)  5 mm
Laser Pulse Energy  100 µJ
Laser Pulse Duration  500 ps
Laser Repetition Rate  50 kHz
Operating Wavelength  1064 nm
Dimensions  229 cm x 132 cm x 209 cm
Weight  Approx. 600 kg

 

Applications

  • Satellite mission support (commercial and scientific)
  • Cross-calibration of navigation satellite systems
  • Satellite geodesy ground station, even at remote locations
  • Monitoring of decommissioned satellites, if equipped with a retro-reflector
    (Space Situational Awareness, SSA)
  • Improved collision warnings for satellites in orbit
  • Space Traffic Management (STM), also for large satellite constellations
    (Space Situational Awareness, SSA)

 


Contact
Oliver Miedaner
Koordinator Wirtschaftskooperationen Region Südwest

Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)

Wirtschaftskooperationen

Stuttgart

Tel.: +49 711 6862-284

Dr. rer. nat. Daniel Hampf
German Aerospace Center

Institute of Technical Physics
, Active Optical Systems
Stuttgart

Tel.: +49 711 6862-751

Fax: +49 711 6862-788

Downloads
Factsheet miniSLR®-System (0.26 MB)
Related Topics
Geophysics
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