A test-bed for space interferometry: Space Platform Interferometer (SPI)The Space Platform Interferometer (SPI), a 20-m two-mirror Michelson interferometer, which can reach magnitude 14 at UV and visible wavelengths, is described. The SPI is attached to a platform serviced from the space station. In addition to its ability to produce unique science in the UV, SPI is intended to demonstrate the feasibility of larger projects in the field. Dynamical behavior of the structure in the gravity gradient environment and fringe stabilization at low photon rate are studied by picking up an adjacent bin (in the near IR) on the same object and using it to track the white light fringe in a separate differential interferometer. The same subsystem also corrects for tilt. Active control of critical parameters ensures optical rigidity. Performances are evaluated in low orbit.
Document ID
19880001258
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Faucherre, M. (Centre National de la Recherche Scientifique Verrieres-Le Buisson (France), United States)
Dame, L. (Centre National de la Recherche Scientifique Verrieres-Le Buisson (France), United States)
Stachnik, R. V. (NASA Headquarters Washington, DC United States)
Traub, W. A. (Harvard-Smithsonian Center for Astrophysics Cambridge, Mass., United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1987
Publication Information
Publication: ESA, ESA Workshop on Optical Interferometry in Space