In an adjustment mechanism for adjusting at least one engine of a spacecraft, including an engine plate for the at least one engine, a pivotable boom for pivoting the engine plate between a retracted position adjacent the spacecraft and at least one extracted position spaced apart from the spacecraft, and a first adjustment drive for pivoting the boom and a second adjustment drive for orienting the engine plate relative to the boom, the first adjustment drive comprises a monoaxial pivoting device comprising a first pivot axis, and the second adjustment drive comprises an at least biaxial pivoting device comprising a second and a third pivot axis, the second or the third pivot axis extending, or being positionable, in parallel with the first pivot axis.
STELLMECHANISMUS ZUM VERSTELLEN WENIGSTENS EINES TRIEBWERKS EINES RAUMFLUGKÖRPERS
REGULATING MECHANISM FOR ADJUSTING AT LEAST ONE ENGINE OF A SPACECRAFT
MECANISME DE REGLAGE D'AU MOINS UNE TURBINE D'UN CORPS SPATIAL
11.10.2017
Patent
Elektronische Ressource
Deutsch
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