equation (6.15) and Fig 6.6 in reflector antennna chapter 6

M.I. Skolnik, “Radar Handbook: Second Edition”, Mc-Graw-Hill Companies, 1990.

Mohamed

I guess not directly - the 10 dB taper rule implies you dont want to get too much energy spilled over the reflector, in case the edges'level is less than 10 dB spillover losses are big. If the edges receive lets say 20dB or more than the center that would mean your reflector ended up too large. Take a look into Balanis book its well covered - spillover and taper losses.

SLL will decrease though if the edges receive lesser power - that means a larger diameter reflector will provide smaller SLL figures.

Dear Pr. Perotoni, 

Thank you for your response. The idea is how to estimate the SLL from space taper using a simple formula? 

There used to be simple graphs in most antenna design books showing sidelobe level as a function of edge illumination.  This is not only due to space attenuation, but also due to the beam-shape of the feed.  See Volakis Antenna Engineering Handbook 4th Ed page 15-22. for example.

A rule of thumb from the graph there is (for a circular aperture)  no taper = 17 dB sidelobes, 10 dB taper = 24 dB sidelobes, 15 dB taper = 30 dB sidelobes, 25 dB taper = 40 dB sidelobes.  The beam gets wider for more edge taper.

Thank you for the answer Mr. Malcolm.

I would like to know more about Space Taper? it's attenuation of electromagnetic waves at edges compared to the center of reflector in space?

Space taper is due to the reduction in power density at longer distances from the feed.  For a parabolic dish with f/d ratio of 4 (the focus is level with the edges of the dish) the edge is twice as far away from the feed as the middle is, and the power density reaching it is 1/4 the power density reaching the centre of the dish.  Reflection at the middle, and in the 45 degree reflector at the edge, doesn't change the power density in either case, so there is a 6 dB space taper at the edge of the aperture even if the feed pattern is uniform in all directions.

Thanks for the explication.

Do you have an idea about ideal value of Space Taper  of 90° corn or cylindrical reflector antenna?

You have to work it out yourself using simple geometry - using the distance from the feed to the part of the reflector you want to know about - to calculate the power density arriving at the reflector, and then using the arrival angle and the angle of the surface to the main beam direction to get the power-density per unit area on the projected area of the reflector.

Thanks