Title :
Space interferometer mission (SIM) instrument design concepts
Author_Institution :
Lockheed Martin, Sunnyvale, CA, USA
Abstract :
SIM is a 12 meter baseline interferometer to be built as part of the NASA Origins program, designed to fly in space and provide high precision astrometry measurements of astronomical objects. SIM will provide angular measurements three orders of magnitude more precise than current space or ground based sensors, allowing the indirect detection of Earth-like planets around neighboring stars. The SIM mission will also include the ability to synthesize images by varying the interferometer baseline lengths and will demonstrate a nulling beam combiner as a technology pathfinder for future missions. A team at Lockheed Martin Missiles and Space (LMMS) in Sunnyvale, CA has been chosen by JPL to enter a partnership to design and build the SIIM instrument. This paper describes the overall LMMS SIM instrument concept and its unique features, including the full aperture laser metrology approach for high precision metrology
Keywords :
astrometry; astronomical telescopes; light interferometers; measurement by laser beam; optical control; physical instrumentation control; Earth-like planets; HOE grating; NASA Origins program; Starlight subsystem; afocal telescopes; angular measurements; beam combiner; full aperture laser metrology; high precision astrometry measurements; indirect detection; instrument design concepts; nulling beam combiner; optical path length differences; real time control; space interferometer mission; technology pathfinder; varied interferometer baseline length; Apertures; Current measurement; Extraterrestrial measurements; Instruments; Metrology; Missiles; NASA; Planets; Space missions; Space technology;
Conference_Titel :
Aerospace Conference, 1999. Proceedings. 1999 IEEE
Conference_Location :
Snowmass at Aspen, CO
Print_ISBN :
0-7803-5425-7
DOI :
10.1109/AERO.1999.789805