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A radio altimeter antenna for a planetary probeThe design of a 400 MHz directional radio altimeter antenna for use in a freely falling probe in a planetary atmosphere is described. It is required that the antenna be physically large to exploit the dependence of the return power on the square of the wavelength. The antenna must be deployable so that it can be stowed behind the heat shield during the phase of atmospheric penetration. The electrical requirement, imposed by the power available and the system noise, is that the gain in the direction of the probe be at least 3 dB over a dipole. The altimeter application imposes the requirement of linear polarization. Dipole elements are impractical because of the proximity of the heat shield, hence monopole elements using the heat shield as an integral part (the ground plane) of the antenna are used. A parasitic element is placed behind the driven element to increase both the front-to-back ratio and the directive gain. The antenna which has been selected has a gain of 4 dB over a dipole, a front-to-back ratio of 8 dB, and a -6 dB beam angle of 34 degrees. Experiments for evaluating the effects of element spacing, length, and tilt angle with respect to the probe axis were conducted on a 1/25 scale model of the antenna at 10 GHz, and impedance measurements were performed on a full scale antenna at 400 MHz.
Document ID
19760040846
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Beyer, J. B.
(Tel-Aviv Univ. Ramat-Aviv, Tel-Aviv, Israel)
Afanasjevs, J.
(Wisconsin, University Madison, Wis., United States)
Levanon, N.
(Tel Aviv University Tel Aviv, Israel)
Date Acquired
August 8, 2013
Publication Date
March 1, 1976
Publication Information
Publication: IEEE Transactions on Antennas and Propagation
Volume: AP-24
Subject Category
Spacecraft Instrumentation
Accession Number
76A23812
Funding Number(s)
CONTRACT_GRANT: NAS5-8015
Distribution Limits
Public
Copyright
Other

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