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Design and applications of a versatile HF radar calibration target in low Earth orbit
Author(s) -
Bernhardt Paul A.,
Siefring Carl L.,
Thomason Joe F.,
Rodriquez Serafin P.,
Nicholas Andrew C.,
Koss Steven M.,
Nurnberger Mike,
Hoberman Chuck,
Davis Matthew,
Hysell David L.,
Kelley Michael C.
Publication year - 2008
Publication title -
radio science
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.371
H-Index - 84
eISSN - 1944-799X
pISSN - 0048-6604
DOI - 10.1029/2007rs003692
Subject(s) - radar , radar cross section , fire control radar , remote sensing , radar engineering details , computer science , satellite , 3d radar , orbit (dynamics) , physics , radar imaging , geology , aerospace engineering , telecommunications , engineering
High frequency (HF) radars are used to detect ionospheric irregularities, meteor trails, and moving targets. The Precision Expandable Radar Calibration Sphere (PERCS) is a simple radar target in space to help determine the operational parameters of ground HF radars. PERCS will have a known radar cross section that is independent of observation direction within 0.5 dB. The PERCS satellite can be launched in a stowed configuration that has about 1 m in diameter. After launch, the PERCS will expand to a diameter of almost 10 m. Upon expansion, a stable wire frame is formed to act as a radar scatter target in the form of a polyhedral sphere. The simplest version of the sphere has 60 vertices (V60) that are joined to 90 rigid segments. Each segment is hinged so that the PERCS can be folded into a compact package for launch. Analysis of the V60 wire frame with a 10 m diameter shows that the radar cross section (RCS) is nearly independent of viewing angle up to 30 MHz. Another design with 240 vertices produces even better performance. Radar systems will be calibrated using the radar echo data and the precise knowledge of the target RCS, position, and velocity. The PERCS can reflect radar signals from natural targets such as field aligned and current driven irregularities not presently accessible from ground‐based radars. The wire frame structure has several advantages over a metalized spheroid “balloon” with (1) much less drag, (2) larger radar cross section, and (3) lower fabrication cost.

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