United States of America As Represented by the Administrator of Nasa

Orbital Sciences Corporation

Steven A Macenka

Russell A Chipman

Herbert A Roeder

Ulli G Hartmann

Robert E Haring

Stephen Charles McClain

Brian J Daugherty

Disclosed herein is a method of determining the near angle scattering of a sample reflective surface comprising the steps of: a) splitting a beam of light having a coherence length of greater than or equal to about 2 meters into a sample beam and a reference beam; b) frequency shifting both the sample beam and the reference beam to produce a fixed beat frequency between the sample beam and the reference beam; c) directing the sample beam through a focusing lens and onto the sample reflective surface, d) reflecting the sample beam from the sample reflective surface through a detection restriction disposed on a movable stage; e) recombining the sample beam with the reference beam to form a recombined beam, followed by f) directing the recombined beam to a detector and performing heterodyne analysis on the recombined beam to measure the near-angle scattering of the sample reflective surface, wherein the position of the detection restriction relative to the sample beam is varied to occlude at least a portion of the sample beam to measure the near-angle scattering of the sample reflective surface. An apparatus according to the above method is also disclosed.

Method and apparatus for measuring near-angle scattering of mirror coatings

The invention provides an imaging spectrometer that provides a wide field-of-view camera and spectrometer for spectral imaging of a large two-dimensional area of the Earth's surface from an orbiting satellite or airplane. The wide field-of-view camera fore-optics includes spherical optical elements arranged monocentrically. The spectrometer includes an all-reflective coupling design that transfers the curved optical image to one or more compact imaging spectrometers. The spectrometers preferably comprise a spherical convex holographic grating and associated reflective optics for dispersing a collimated optical beam into its spectral components and focusing the spectral image onto a planar detector array. The instrument described herein is designed to operate in a 'pushbroom' fashion, that is, the forward motion of the satellite or airplane generates the spatial dimension of the resulting image. Because of its compact optical design and because no additional scanning equipment is required to scan the Earth's surface, the instrument is very compact and light-weight.

Wide field-of-view imaging spectrometer

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Altadena, CA, United States of America

Steven A Macenka