Abstract
The design of a 400 MHz directional antenna for a space vehicle is presented. The design utilizes the spacecraft itself as an integral part of the antenna. The antenna 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°. Design equations and experimental data are presented.
Original language | English |
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Pages (from-to) | 206-208 |
Number of pages | 3 |
Journal | IEEE Transactions on Antennas and Propagation |
Volume | 24 |
Issue number | 2 |
DOIs | |
State | Published - Mar 1976 |