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Astrophysical Adaptation of Points, the Precision Optical Interferometer in SpacePOINTS (Precision Optical INTerferometer in Space) would perform microarcsecond optical astrometric measurements from space, yielding submicroarcsecond astrometric results from the mission. It comprises a pair of independent Michelson stellar interferometers and a laser metrology system that measures both the critical starlight paths and the angle between the baselines. The instrument has two baselines of 2 m, each with two subapertures of 35 cm; by articulating the angle between the baselines, it observes targets separated by 87 to 93 deg. POINTS does global astrometry, i.e., it measures widely separated targets, which yields closure calibration, numerous bright reference stars, and absolute parallax. Simplicity, stability, and the mitigation of systematic error are the central design themes. The instrument has only three moving-part mechanisms, and only one of these must move with sub-milliradian precision; the other two can tolerate a precision of several tenths of a degree. Optical surfaces preceding the beamsplitter or its fold flat are interferometrically critical; on each side of the interferometer, there are only three such. Thus, light loss and wavefront distortion are minimized. POINTS represents a minimalistic design developed ab initio for space. Since it is intended for astrometry, and therefore does not require the u-v-plane coverage of an imaging, instrument, each interferometer need have only two subapertures. The design relies on articulation of the angle between the interferometers and body pointing to select targets; the observations are restricted to the 'instrument plane.' That plane, which is fixed in the pointed instrument, is defined by the sensitive direction for the two interferometers. Thus, there is no need for siderostats and moving delay lines, which would have added many precision mechanisms with rolling and sliding parts that would be required to function throughout the mission. Further, there is no need for a third interferometer, as is required when out-of-plane observations are made. An instrument for astrometry, unlike those for imaging, can be compact and yet scientifically productive. The POINTS instrument is compact and therefore requires no deployment of precision structures, has no low-frequency (i.e., under 100 Hz) vibration modes, and is relatively easy to control thermally. Because of its small size and mass, it is easily and quickly repointed between observations. Further, because of the low mass, it can be economically launched into high Earth orbit which, in conjunction with a solar shield, yields nearly unrestricted sky coverage and a stable thermal environment.
Document ID
19970004991
Acquisition Source
Headquarters
Document Type
Contractor Report (CR)
Authors
Reasenberg, Robert D.
(Smithsonian Astrophysical Observatory Cambridge, MA United States)
Babcock, Robert W.
(Smithsonian Astrophysical Observatory Cambridge, MA United States)
Murison, Marc A.
(Smithsonian Astrophysical Observatory Cambridge, MA United States)
Noecker, M. Charles
(Smithsonian Astrophysical Observatory Cambridge, MA United States)
Phillips, James D.
(Smithsonian Astrophysical Observatory Cambridge, MA United States)
Schumaker, Bonny L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Ulvestad, James S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
McKinley, William
(Itek Optical Systems Lexington, MA United States)
Zielinski, Robert J.
(Itek Optical Systems Lexington, MA United States)
Lillie, Charles F.
(TRW Defense Systems Group Redondo Beach, CA United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1996
Subject Category
Optics
Report/Patent Number
NAS 1.26:202669
NASA-CR-202669
Report Number: NAS 1.26:202669
Report Number: NASA-CR-202669
Accession Number
97N12978
Funding Number(s)
CONTRACT_GRANT: NAGw-4768
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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