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Radar System Engineering

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SEC. 9.25] EXAMPLES OF RADOMES 317<br />

will determine whether the problem is one of strength or stability. The<br />

stability problem is a difficult one to meet, since no ribs or other means<br />

of reinforcement can be used for the extensive transparent area because<br />

of possible distortion of the electrical pattern.<br />

The design of the mounting of the radome should have due consideration.<br />

Servicing requirements necessitate removal of the radome. The<br />

means of mounting the radome must be quick-fastening as well as strong.<br />

Just as the final proof of a satisfactory aerodynamical and electrical<br />

design are aerodynamical and electrical tests, so structural tests are<br />

FIc. 9.3S.—A retractable radome (1) partly extended on a B-29, and tbe bulge to accom.<br />

modate tbe r-f unit (2) aft of the radome.<br />

necessary to assure a satisfactory design, for in a streamlined shape the<br />

calculations can at best be only approximate.<br />

9.26. Examples of Radomes.—Types of radomes vary greatly in size,<br />

shape, and method of construction. Attention is called to a few representative<br />

radomes.<br />

Figure 9.38 shows an early type of retractable airborne radome<br />

mounted on a B-29. The radome is a cylinder 3% in. in diameter and<br />

extending about 33 in. when unretracted. While the shape is ideal<br />

electrically, its effect on the speed of the aircraft is most objectionable.<br />

The leading edge of the Eagle vane (Fig. 9“18) is a radome made of<br />

two Fiberglas walls with occasional ribs as spacers. While the airfoil<br />

section is in itself of low drag, the attachment to the plane increases the<br />

drag until it is almost as high as that for the cylindrical radome. This<br />

increase in drag is due to the interference and stagnation points set up by<br />

mounting the airfoil to the plane. An additional feature of this radome<br />

was that it was designed to be deiced by means of hot air. The optimum<br />

wall spacings for heat transfer and for electrical transmission do not<br />

coincide, so that deicing is not very efficient.<br />

A good bombing antenna installation for a B-29 is shown in Fig. 9.39.<br />

This radome houses the antenna shown in Fig. 9.8. The radome extends

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