Persistent Identifier
|
hdl:2014/40754 |
Publication Date
|
2004-06-22 |
Title
| Prototype development of a Geostationary Synthetic Thinned Aperture Radiometer, GeoSTAR |
Author
| Tanner, Alan B. (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004.)
Wilson, William J. (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004.)
Kangaslahti, Pekka P. (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004.)
Lambrigsten, Bjorn H. (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004.)
Dinardo, Steven J. (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004.)
Piepmeier, Jeffrey R. (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004.)
Ruf, Christopher S. (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004.)
Rogacki, Steven (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004.)
Gross, S.M. (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004.)
Musko, Steve (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004.) |
Point of Contact
|
Use email button above to contact.
Tanner, Alan B. |
Description
| Preliminary details of a 2-D synthetic aperture radiometer prototype operating from 50 to 58 GHz will be presented. The instrument is being developed as a laboratory testbed, and the goal of this work is to demonstrate the technologies needed to do atmospheric soundings with high spatial resolution from Geostationary orbit. The concept is to deploy a large sparse aperture Y-array from a geostationary satellite, and to use aperture synthesis to obtain images of the earth without the need for a large mechanically scanned antenna. The laboratory prototype consists of a Y-array of 24 horn antennas, MMIC receivers, and a digital cross-correlation sub-system. System studies are discussed, including an error budget which has been derived from numerical simulations. The error budget defines key requirements, such as null offsets, phase calibration, and antenna pattern knowledge. Details of the instrument design are discussed in the context of these requirements. |
Subject
| Other |
Production Date
| 2004-06-22 |