proposed single open reflector for the galileo mission

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SLR Tracking of GNSS Constellations, Metsovo 2009 Proposed Single Open Reflector for the GALILEO Mission R.Neubert formerly with GFZ Potsdam, Germany, [email protected] J.Neubert IB Neubert GmbH, Zurich, Switzerland, [email protected] J.Munder SpaceTech GmbH, Immenstaad, Germany, [email protected] L.Grunwaldt GFZ German Research Centre for Geosciences, Potsdam, Germany [email protected]

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Page 1: Proposed Single Open Reflector for the GALILEO Mission

SLR Tracking of GNSS Constellations, Metsovo 2009

Proposed Single Open Reflector for theGALILEO Mission

R.Neubert formerly with GFZ Potsdam, Germany, [email protected]

J.Neubert IB Neubert GmbH, Zurich, Switzerland, [email protected]

J.Munder SpaceTech GmbH, Immenstaad, Germany, [email protected]

L.Grunwaldt GFZ German Research Centre for Geosciences, Potsdam, Germany

[email protected]

Page 2: Proposed Single Open Reflector for the GALILEO Mission

SLR Tracking of GNSS Constellations, Metsovo 2009

Far Field of the GALILEO Prism Array

Single prism

Average

velocity aberration 23.7....24.2 µrad

50 25 0 25 500

250

500

750

1000cross section (84 prims)

µrad

Mill

ion

sqm

Page 3: Proposed Single Open Reflector for the GALILEO Mission

SLR Tracking of GNSS Constellations, Metsovo 2009

circular array, radius R=25cm, angle of incidence:

Single shot precision:

α=12°

Normal point precision:

σ = 2.6cm (12°)

σ resσ

N

σR2

sin α( )⋅

Expected Signature of the GALILEO Array

25 measurements required to get 5mm precision

Page 4: Proposed Single Open Reflector for the GALILEO Mission

SLR Tracking of GNSS Constellations, Metsovo 2009

Page 5: Proposed Single Open Reflector for the GALILEO Mission

SLR Tracking of GNSS Constellations, Metsovo 2009

The Proposed Open Reflector Geometry

Main Features of the Reflector:

•no pulse spreading•high effective radar cross section•small (up to 20cm diam. front face)•low weight

Page 6: Proposed Single Open Reflector for the GALILEO Mission

SLR Tracking of GNSS Constellations, Metsovo 2009

Far Field of the Open Reflector with Conical Wave Front

F

40 20 0 20 400

200

400

600cross section

µrad from center

Mill

ion

sqm

Wave front

Far Field

Page 7: Proposed Single Open Reflector for the GALILEO Mission

SLR Tracking of GNSS Constellations, Metsovo 2009

Conical Shape of the Mirrors

difference to perfect LRRin µm

remaining deformation afterintroducing 2.1arsec offsets

Page 8: Proposed Single Open Reflector for the GALILEO Mission

SLR Tracking of GNSS Constellations, Metsovo 2009

Wave Front and Far Field from ASAP, α=0°

Page 9: Proposed Single Open Reflector for the GALILEO Mission

SLR Tracking of GNSS Constellations, Metsovo 2009

Wave Front and Far Field from ASAP, α=12°

Page 10: Proposed Single Open Reflector for the GALILEO Mission

SLR Tracking of GNSS Constellations, Metsovo 2009

Far Field: Dependence on Orientation

α=6°

α=12°

0° 30° 60° Azimuth

Page 11: Proposed Single Open Reflector for the GALILEO Mission

SLR Tracking of GNSS Constellations, Metsovo 2009

Thermal Simulations of Orbital Heat Loads

Prelim inary Results, Designwill be further optim zed

• High transient variation of theaverage temperature is approx.20°C (blue line)

• Low spatial variation ofapprox. 4.5°C at 6000sec shortlyafter eclipse phase from45967sec to 1619sec (red line)

Color-coded temperature plot, Red = -35°CBlue = -39°C

Partial SunHeating shortlyafter Eclipse

Zerodur mirror, high-reflective dielectricalcoating, centered @532nm

Page 12: Proposed Single Open Reflector for the GALILEO Mission

SLR Tracking of GNSS Constellations, Metsovo 2009

Conclusion

The proposed open reflector is advantageous compared to the standard prism arraybecause of:

•no pulse spreading at all angles•equal or higher effective cross section but smaller dimension (higher antenna gain)•at low elevation (high angle of incidence) a single received photon is needed only to achieve the full resolution of the SLR system

Main problem area:thermal distortion caused by sun heating should be kept small by the use of selected Zerodur substrate, dielectric coating and sun shield