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Lampoldshausen
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ARD
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Meteosat Bipropellant Propulsion
Satellite and spacecraft propulsion systems from Astrium Lampoldshausen
Image gallery of the Meteosat bipropellant unified propulsion system:
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Design Life:
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7 years.
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Meteosat
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Dry Mass:
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1072 kg
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Launch mass:
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2050 kg.
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Launcher:
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Ariane 5.
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Spin rates:
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55 rpm - transfer GTO to GEO.
100 RPM IN GEO.
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Power demand:
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500 W.
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Propulsion:
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Bipropellant UPS.
2 X 400 N liquid apogee engines.
6 x 10 N reaction control thrusters.
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Payload:
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12 channel enhanced imaging and
pseudo sounding radiometer.
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Flight models:
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3
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Meteosat Unified Propulsion System - 2nd Generation.
Meteosat Unified Propulsion System - FM3 Acceptance Tests.
Meteosat Unified Propulsion System - FM3 Acceptance Tests.
Contact for Further Information
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If
you require more detailed information on any of our products or services,
then please contact
us, indicating your particular areas of interest or intended application.
Your enquiry will receive our best attention.
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