. The Bell System technical journal . Fig. 60—AX/.\PS-4 Antenna. The SCR-520, SCR-717 and SCR-720 Antennas- The antenna shown in Fig. ol is typical of the type used with the SCR-520and SCR-720 aircraft interception (night fighter) airborne radar equip-ment, as well as the SCR-717 sea search and anti-submarine airborne radarequipment. The parabolic reflector is 29 inches in diameter and produces aradiation beam about 10° wide. The absolute gain is approximately 25db. RF energy is supplied to a pressurized emitter through a pressurizedtransmission line system which includes a rotary joint l


. The Bell System technical journal . Fig. 60—AX/.\PS-4 Antenna. The SCR-520, SCR-717 and SCR-720 Antennas- The antenna shown in Fig. ol is typical of the type used with the SCR-520and SCR-720 aircraft interception (night fighter) airborne radar equip-ment, as well as the SCR-717 sea search and anti-submarine airborne radarequipment. The parabolic reflector is 29 inches in diameter and produces aradiation beam about 10° wide. The absolute gain is approximately 25db. RF energy is supplied to a pressurized emitter through a pressurizedtransmission line system which includes a rotary joint located on the ver-so Written by J. F. Morrison, 314 BELL SYSTEM TECHNICAL JOURNAL tical axis and a tilt joint on the horizontal axis. Either vertical or hori-zontal polarization can be used by rotating the mounting position of theemitter. Vertical polarization is preferred for aircraft interception workand horizontal polarization is i)referred for sea search Fig. 61—SCR-520 Antenna. For aircraft interception the military services desired to scan rapidly alarge solid angle forward of the pursuing airplane, 90° right and left, 15°below and 50° above the line of flight. The data is presented to the opera-tor in the form of both B and C })resentations and for this purposepotentiometer data take-offs are provided on the antenna. The reflectoris spun on a vertical axis at a rate of 360 rpm and at the same time it is RADAR ANTENNAS 315 made to nod up and down about its horizontal axis by controllable amountsup to a total of 65° and at a rate of 30° per second. In the sea search SCR-717 equipment, selsyn azimuth position data take-offs are provided which drive a PPI type of indicator presentation. Therotational speed about the vertical axis in this case is either 8 or 20 rpmas selected by the operator. The reflector can also be tilted about itshorizontal axis above or below the line of flight as desired by the operator. It wUl be note


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Keywords: ., bookcentury1900, bookdecade1920, booksubjecttechnology, bookyear1