Optical interferometer systems in space: Configuration and structure concepts using space rigidized elements

Statistics – Applications

Scientific paper

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Inflatable Structures, Self Erecting Devices, Space Erectable Structures, Very Long Base Interferometry, Ariane Launch Vehicle, Optical Measuring Instruments, Space Observations (From Earth)

Scientific paper

The use of inflatable space-rigidized structures for use in orbital optical interferometry systems is discussed. Their ability to provide 100 m long supporting elements for such interferometers is analyzed. It is found that such systems can be built and packaged for launch to geostationary orbit by Ariane 5 with specific masses of 0.8 to 1.8 kg/m. They can be stiff enough to be controllable, and provide interfaces for observing telescopes sufficiently free of vibration for sensor scanning frequencies. The use of such optical interferometric methods is discussed.

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