Radar System Engineering

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578 PRIME POWER SUPPLIES FOR RADAR [SEC. 14.6 that would generate a frequency above resonance, the machine speed would continue to increase, being limited only by friction and windage losses. CentrifWal Control.—The most recent method of speed regulation to be used on aircraft inverters is a carbon-pile governor as used by the Holtzer-Cabot Electric Company. It is shown in Fig. 14.20 and also in Fig. 14.21 mounted on a 750-va PU-16 inverter. The electrical connections are shown in the schematic diagram Fig. 14.22. A centrifugal device on the end of the inverter shaft acts against the carbon pile in such a manner that increased speed will reduce the m-essure on the carbon pile and reduced speed will increase the pressure. As shown in Fig. 14.20, when the machine is at rest the carbon pile is held in compres- Alternator fwld h filter Contactor .. A L~~~ .Itemator Cabwle I ;,S1l, ~ ,;gt FIG. 14.22.4chematic T A-c Ofi 1 fifter = %ries fwld Voltage adwstmg “’’’t”’ -f-l&q . diagram of Wincharger PU-16 aircraft inverter, 750va, 115volts, 400Cps. sion by the large coil spring in the rotating element. The resistance is then least, giving maximum field for good starting characteristics. As the machine speed increases, the centrifugal weights compress the spring and reduce the pressure on the pile, increasing its resistance. Should the machine exceed its rated speed, the carbon pile will be compressed by the spring under the adjusting screw. At rated speed, the carbon pile is balanced between these two springs and a slight change in speed will cause a relatively large change in resistance. Springs A and B position the tube holding the carbon pile. I Electronic Speed Controls.—The Eclipse-Pioneer Division of Bendix Aviation has recently developed an electronic speed control for use on motor alternator sets of 1500-va capacity and larger. This regulator is designed to hold speed within the limits of Army-Navy Specification AN-I-lo. 1C. T. Button, “.4 Carbon-pile Speed Governor, ” A lEE Transactions, 65, 4 (January 1946).
SEC. 14.7] DYNAMOTORS 579 14.7. Dynamotors.—To supply smaller radar sets with moderate power at not over 1000 or 1200 volts, a dynamotor is often more economical in weight and efficiency than an inverter. A dynamotor has conventional d-c shunt- and series-field windings on the stator and one or more armature windings on the rotor. The rotor winding is excited through brushes and a commutator from the input voltage. A single rotor winding can be tapped to give the required secondary voltage. Alternatively, separate rotor windings can be used, with turns-ratios to the primary winding chosen to provide the correct output voltages. The required d-c voltages are brought out through commutators from the secondary windings. Dynamotors have been built i FIG. 14.23 .—Eicor Inc. aircraft dynamotor, to give voltages as high as 2000 volts, but such machines meet severe difficulties with commutation and insulation. Dual- and triple-output dynamotors are very common, and several machines having four outputs (Fig. 14.23) have been built, but it is impractical to go beyond this because of the large number of windings and commutators involved. Dynamotors for military aircraft are built for an input voltage of 27.5 volts. For automobiles, commercial aircraft, and miscellaneous use, dynamotcrs are built for input voltages of 6, 12, 32, and 110 volts. Output ratings vary from 14 or less to over 1200 volts, and from 30 ma to 5 amp, with any combination of two, three, or four at a time. Weights vary from 5 lb, for a total output of 20 watts, to 26 lb, for an output of 400 watts. Efficiencies range from 40 per cent to 60 per cent. The dynamotor suffers from poor regulation. Furthermore, variations in input voltage may be as great as 10 per cent. The dynamotor
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CHAPTER 1 INTRODUCTION BY LOUIS N.
Page 4 and 5:
4 IN TRODUC7”ION [SEC.1.2 flik~c
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6 INTRODUCTION [SEC.1.3 pulse leaki
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8 INTRODUCTION [SEC.1.4 antenna is
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10 INTRODUCTION [SEC.14 step in out
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12 INTRODUCTION [SEC.1.5 where high
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14 INTRODUCTION [SEC.1.6 England, F
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16 INTRODUCTION [SEC.1°7 Microwave
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CHAPTER 2 THE lU.DAR EQUATION BY E.
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20 THE RADAR EQUATION [SEC.22 radia
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22 THE RADAR EQUATION [SEC.25 Again
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24 THE RADAR EQUATION [SEC.2.5 time
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26 THE RADAR EQUATION [SEC.2.5 smal
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28 THE RADAR EQUATION [SEC.!2.7 lim
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30 THE RADAR EQUATION [SEC.28 Anoth
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32 THE RADAR EQUATION [SEC.28 first
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34 TIIE RADAR EQUATION [Sm. 29 the
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36 THE RADAR EQUATION [SEC.2.10 (Vo
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38 THE RADAR EQUATION [SEC.210 prac
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40 THE RADAR EQUATION [SEC.2.10 tai
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42 THE RADAR EQUATION [SEC.2.11 swe
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44 THE RADAR EQUATION [SEC.2.11 res
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46 THE RADAR EQUATION [SEC.211 Alth
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48 THE RADAR EQUATION [SEC.212 othe
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50 THE RADAR EQUATION [SEC.212 The
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52 THE RADAR EQUATION [SEC. 2.12 Th
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54 THE RADAR EQUATION [SEC.213 smal
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56 THE RADAR EQUATION [SEC. 2.14 an
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58 THE RADAR EQUATION [SEC.2.15 not
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60 TIIE RADAR EQUATION [SEC.2.15 wt
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62 THE RADAR EQUATION [SEC.215 per
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64 PROPERTIES OF RADAR TARGETS [SEC
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66 PROPERTIES OF RADAR TARGET,S [SE
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PROPERTIES OF RADAR TARGETS [SEC.37
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Page 88 and 89:
88 PROPERTIES OF R.41~.l R T.-lRGE~
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92 PROPERTIES OF RA1l.4R TARGETS [S
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SEC.315] STRUCTURES 99 example, the
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SF,C. 3.16] CITIES 101 reflection w
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SEC. 3.16] CITIES 103 signal repres
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SEC. 3.16] CITIES 105 four signals
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108 PROPERTIES OF RADAR TARGETS [SE
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112 PROPERTIES OF RADAR TARGETS [SE
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CHAPTER 4 LIMITATIONS OF PULSE RADA
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118 LIMITATIONS OF PULSE RADAR [SEC
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122 LIMITATIONS OF PC’LSE RADAR [
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Page 128 and 129:
128 C-W RADAR SYSTEMS [SEC. 5.1 tar
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130 C-W RADAR SYSTEMS [sm. 53 point
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132 C-W RADAR S’YSTEMS [SEC.56 bi
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134 C-W RADAR SYSTEMS [SEC. 56 tran
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136 C-W RADAR SYSTEMS [SEC. 5.6 int
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138 C-W RADAR SYSTEMS [SEC, 5.6 rel
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140 C-W RADAR SYSTEMS [SEC 37 and j
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142 C-II’ RADAR SYSTEMS [SEC. 57
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144 C-W RADAR SYSTE.JfS [SEC. 58 gi
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146 C-W RADAR SYSTEMS [SEC. 58 Modu
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148 C-T RA DAR S YSTE.lf S [SEC. 59
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150 C-W RADAR SYSTEMS [SEC. 5.11 cy
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152 C-W RADAR SYSTEMS [SEC.5.11 Now
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154 C-W RADAR SYSTEMS [SEC.5.11 exc
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156 C-W RADAR SYSTEMS [SEC. 5.11 in
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158 C-W RADAR SYSTEMS [SEC. 5.12 Pu
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CHAPTER 6 THE GATHERING AND PRESENT
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162 THE GATHERING AND PRESENTATION
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Page 168 and 169:
168 THE GATHERING AND pRESENTA TION
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~70 THE GATHERING AND PRESENTA TION
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SEC. 66] PLANE DISPLAYS INVOLVING E
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SEC. 69] IiARLY AIRCRAFT-WARNING RA
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SEC. 69] EARLY AIRCRAFT-WARNING RAD
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f$Ec. 69] EARLY AIRCRAFT-WARNING RA
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SEC. 6.9] EARLY AIRCRAFT-WARNING RA
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SEC. 6.10] PPI RADAR FOR SEARCH, CO
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SEC. 6.11] HEIGHT-FINDING INVOLVING
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SEC.6.12] HEIGHT-FINDING WITH A FRE
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- - -— . .. —-— - .. —-.
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SEC. 612] HEIGHT-FINDING J~ITH A FR
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SEC. 6.13] HOMING 197 ber of the pa
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SEC.6.13] HOMING 199 usually made t
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SEC. 6.13] HOMING 201 application,
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SEC. 6.14] PRECISION TRACKING OF A
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SEC.6.14] PRECISION TRACKING OF A S
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SEC. 614] PRECISION TRACKING OF A S
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f$Ec. 614] PRECISION TRACKING OF A
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SEC. 615] PRECISION TRACKING DURING
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CHAPTER 7 THE EMPLOYMENT OF RADAR D
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SEC.72] AIDS TO INDIVIDUAL NAVIGATI
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SEC. 7.2] AIDS TO INDIVIDUAL NAVIGA
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SEC. 73] AIDS TO PLOTTING AND CONTR
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SEC.7.3] AIDS TO PLOTTING AND CONTR
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SEC.7.3] AIDS TO PLOTTING AND CONTR
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SEC. 7.4] THE RELAY OF RADAR DISPLA
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SEC. 7.51 RA DAR IN THE RAF FIGHTER
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SEC. 7.6] THE U.S. TACTICAL AIR COM
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SEC.7.6] THE U.S. TACTICAL AIR COMM
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238 THE EMPLOYMENT OF RA DAR DATA [
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240 THE EMPLOYiWENT OF RADAR DATA [
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242 THE EMPLOYMENT OF RADAR DATA [S
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244 RADAR BEACONS [SEC. 8 duration
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246 RADAR BEACONS [SEC. 8.1 beacons
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248 RADAR BEACONS [SEC.8.1 4. Porta
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250 RADAR BEACONS [SEC.8.2 Table 8.
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252 RADAR BEACONS [SEC.84 restricte
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254 RADAR BEACONS [SEC. 85 radar se
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256 RADAR BEACONS [SEC.85 In the ca
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258 It Al)AIt BEACONS [S,,c, S3 Sim
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SEC. 86] FREQUENCY CONSIDERATIONS 2
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SEC. 87] INTERR~A TION CODES 263 wi
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SEC. 8.9] TRAFFIC CAPACITY 265 diff
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SEC.8.9] TRAFFIC CAPACITY 267 which
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270 RADAR BEACONS [SEC. 810 range a
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272 ANTENNAS, SCANNERS, A.VD STABIL
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274 ANTENNAS, SCANNERS, AND ST ABIL
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276 ANTENNAS, SCANNERS, AND STABILI
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SEC. 913] THE AN/APQ-7 (EAGLE) SCAN
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SEC.913] THE AN/APQ-7 (EAGLE) SCANN
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SEC. 9.14] SCHWA RZSCHILD ANTENNA 2
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SEC. 9.14] SCH WA RZSCHILD ANTENNA
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SEC. 9.15] SCI HEIGHT FINDER 299 de
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SEC.9.15] SCI HEIGHT FINDER 301 In
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SEC.916] OTHER TYPES OF ELECTRICAL
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SEC,9.17] STABILIZATION OF THE BEAM
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SEC. 9.17] STABILIZATION OF’ THE
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SEC. 9.17] STABILIZATION OF THE BEA
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t$Ec. 9,18] DATA STABILIZATION 311
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SEC. 920] INSTALLATION OF SURFACE-B
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SEC. 922] STREA MLIA”ING 315 func
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SEC. 9.25] EXAMPLES OF RADOMES 317
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SEC.9.25] EXAMPLES OF RADOMES 319 a
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SEC. 10.1] CONSTRUCTION 321 of the
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SEC. 10.1] CONSTRUCTION 323 later r
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SEC.10.2] THE RESONANT SYSTEM 325 m
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SEC. 1021 THE RESONANT SYSTEM 327
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SEC. 10.2] THE RESONANT SYSTEM 329
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SEC. 103] ELECTRON ORBITS AIVD THE
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SEC. 103] ELECTRON ORBITS AND THE S
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SEC. 103] ELECTRON ORBITS AND THE S
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SEC. 10.4] PERFORMANCE CHARTS AND R
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SEC. 10.4] PEIWORMilNCE CHARTS AND
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SEC. 10.5] MAGNETRON CHARACTERISTIC
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SEC.105] MAGNETRON CHARACTERISTICS
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SEC. 105] MAGNETRON CHARACTERISTICS
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SEC. 10.5] MAGNETRON CHARACTERISTIC
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SEC. 10.6] MAQNETRON CHARACTERISTIC
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L%C. 10.6] MAGNETRON CHARACTERISTIC
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SEC. 10.7] PULSER CIRCUITS 357 and
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SEC. 10.7] PULSER CIRCUITS 359 tude
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SEC. 10.7] PULSER CIRCUITS 361 cen~
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SEC. 108] LOAD REQUIREMENTS 363 TAB
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SEC. 10.8] LOAD REQUIREMENTS 365 to
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SEC. 109] THE HARD-TUBE P ULSEh? 36
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SEC. 10.9] THE HARD-TUBE P ULSER 36
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SEC 10.9] THE HARD-lUBE PULSER 371
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Sl?lc.10.91 LINE-TYPE PULSERS 373 D
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SEC. 10,10] LINE-TYPE PULSERS 375 i
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SEC. 10.10] LINE-TYPE PULSERS 377 I
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SEC. 10.10] LINE-T YPE PULSERS 379
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SEC. 10.10] LINE-TYPE PULSERS 381 T
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SEC.10.11] MISCELLANEOUS COMPONENTS
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SEC. 1011] MISCELLANEOUS COMPONENTS
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R-F CHAPTER 11 COMPONENTS BY A. E.
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SEC.11.2] COAXIAL LINES 393 Why a M
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SEC.11.2] COAXIAL LINES 395 lines h
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SEC.11.2] COAXIAL LINES 397 since n
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SEC,113] JVA VEGUIDE 399 than a qua
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i?EC. 11.3] WA VEGUIDE 401 too grad
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SEC. 113) WA VEGUIDE 403 types of m
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SEC. 11.4] RESONANT CAVITIES 405 co
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SEC. 11.5] D,C”PLEXING AND TR SWI
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SEC. 115] DUPLEXING AND TR SWITCHES
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SEC. 11.5] DUPLEXING AND TR SWITCHE
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SEC.11.6] THE MIXER CRYSTAL 413 sem
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SEC. 11.7] THE LOCAL OSCILLATOR 415
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SEC. 11 .8] THE MIXER 417 minimum l
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SEC.11.10] REASONS FOR AN R-F PACKA
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SEC. 11.11] DESIGN CONSZDERA TZONS
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SEC.11.11] DESIGN CONSIDERATIONS FO
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SEC. 11.12] ILLUSTRATIVE EXAMPLES O
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SEC. 11°12] ILL US’TRA TIVE EXAM
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SEC. 11.12] ILL USTRA TIVE EXAMPLES
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SEC.11.12] ILL US1’IiA TI VE EXA
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CHAPTER 12 THE RECEIVING SYSTEM—R
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SEC. 122] A TYPICAL RECEIVING SYSTE
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SEC.12.2] A TYPICAL RECEIVING SYSTE
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SEC. 122] A TYPICAL RECEIVING SYSTE
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SEC.12.3] SPECIAL PROBLEMS IN RADAR
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SEC.12.4] I-F AMPLIFIER DESIGN 443
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SEC.12.4] I-F AMPLIFIER DESIGN 445
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SEC.124] I-F AMPLIFIER DESIGN 447 i
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SEC. 125] SECOND DETECTOR 449 This
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SEC.12.6] VIDEO AMPLIFIERS 451 ampl
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SEC.12.7] A UTOMA TIC FREQUENCY CON
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SEC. 12.7] A UTOMA TIC FREQUENCY CO
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S~C. 128] PROTECTION AGAINST EXTRAN
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SEC. 128] PROTECTION AGAINST EXTRAN
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SEC. 12.8] PROTECTION AGAINST E-YTR
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&- L,-self resonant COIIS at mterme
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J All resistors~ watt Interstate co
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SEC. 12.10] LIGHTH”EIGIIT AIRBOR.
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s, 0.001 $180 b To reflector To sea
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+ 180v T +120V 470 470 470 470 e“
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SEC.12.11] AN EXTREMELY WIDEBAND RE
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CHAPTER 13 THE RECEIVING SYSTEM—I
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SEC.13.1] ELECTRICAL PROPERTIES OF
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SEC 13.2] CATHODE-RAY TUBE SCREENS
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SEC.13.2] CATHODE-RAY TUBE SCREENS
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SEC. 13.3] SELECTIO.V OF THE CATHOD
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SEC. 13.3] SELECTION OF THE CATHODE
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SEC. 13.4] ANGLE-DATA TRANSMITTERS
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SEC.13.4] ANGLE-DATA TRANSMITTERS 4
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SEC. 13.5] ELECTROMECHANICAL REPEAT
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SEC. 13.6] AMPLIFIERS 493 whence th
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SEC. 13.6] AMPLIFIERS 495 by using
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SEC. 13.7] GENERA TION OF RECTANGUL
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SEC. 13.7] GENERATION OF RECTANGULA
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. SEC. 13.8] GENERA TION OF SHARP P
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SEC. 139] ELECTRONIC SWITCHES 503 T
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SEC. 13.9] ELECTRONIC SWITCHES 505
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SEC. 13.9] ELECTRO.VIC ISWI TCHES 5
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SEC. 13.9] ELECTRONIC SWITCHES 509
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SEC. 1310] SAWTOOTH GENERATORS 511
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SEC.13.10] SAWTOOTH GE,VBliATOh?S 5
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SEC. 1311] ANGLE INDICES 515 bright
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SEC. 13.11] ANGLE INDICES 517 the s
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. . “4 100k.lw $4.7k-lw .& t, T 0
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SEC.K3.121 RANGE AND HEIGIiT INDICE
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i%C.13121 RANGE AND HEIGHT INDICES;
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SEC. 13.13] DESIGN OF A-SCOPES 525
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Page 529 and 530: SEC.1314] B-SCOPE DESIGN 529 \
Page 531 and 532: SEC. 13.14] B-SCOPE DESIG.V 531 wil
Page 533 and 534: Trigger I I I (CT)Sawtooth —. (A)
Page 535 and 536: SEC.1316] RESOLVED TIME BASE PPI 53
Page 537 and 538: SEC. 13.16] RESOLVED mi? TIME BASE
Page 539 and 540: SEC. 13.17] RESOLVED-CURRENT PPI 53
Page 541 and 542: SEC. 13.17] RESOLVED-CURRENT PPI 54
Page 543 and 544: + 200V— — — J 60k . Llk )k 60
Page 545 and 546: SEC. 13.19] 1’HE RANGB-ll EIGII1
Page 547 and 548: SEL!. 13.19] THE RANGE-HEIGHT INDIC
Page 549 and 550: SEC. 13.20] RESOLUTION AND CONTRAST
Page 551: SEC. 13.211 SPECIAL RECEIVING TECHN
Page 554 and 555: 554 THE RECEIVING SYSTEM-INDICATORS
Page 556 and 557: 556 PRIME POWER SUPPLIES FOR RADAR
Page 558 and 559: . . . 0.9 P~- 860-’CPS CF over 2
Page 562 and 563: 562 PRIME POWER SLTPPLIES FOR RADAR
Page 572: 572 PRIME POWER SUPPLIES FOR RADAR
Page 575 and 576: SEC. 14.6] SPEED REGULATORS 575 ‘
Page 577: SEC. 146] SPEED REGULATORS 577 havi
Page 581 and 582: SEC.14.8] VIBRATOR POWER SUPPLIES 5
Page 583 and 584: SEC. 1410] FIXED LOCATIONS 583 port
Page 585 and 586: SEC. 14.13] ULTRAPORTABLE UNITS 585
Page 587 and 588: SEC. l’k~~] SHIP RADAR SYSTEMS 58
Page 589 and 590: SEC. 151] INTRODCCTIO,\- 589 the pr
Page 591 and 592: SEC, 152] NEED FOR SYSTEM TESTING 5
Page 593 and 594: SEC, 153] INITIAL PLANNING AND OBJE
Page 595 and 596: SEC. 15.4] THE RANGE EQUATION 595 n
Page 597 and 598: SEC. 15.5] CHOICE OF PULSE LENGTH 5
Page 599 and 600: SEC. 15.7] AZIMUTH SCAN RATE 599 to
Page 601 and 602: SEC. 15.8] CHOICE OF BEAM SHAPE 601
Page 603 and 604: SEC. 15.8] CHOICE OF BEAM SHAPE 603
Page 605 and 606: SEC. 15.9] CHOICE OF WAVELENGTH 605
Page 607 and 608: SEC. 15.10] COMPONENTS DESIGN 607 1
Page 609 and 610: SEC.16.11] MODIFICA TIO.VS A,YD ADD
Page 611 and 612: SEC. 15.12] DESIGN OBJECTIVES AND L
Page 613 and 614: SEC. 15.12] DESIGN OBJECTIVES AND L
Page 615 and 616: SEC. 15.13] GENERAL DESIGN OF THE A
Page 617 and 618: SEC. 15.14] DETAILED DESIGN OF THE
Page 619 and 620: SEC. 15.14] DETAILED DESIGN OF THE
Page 621 and 622: ,/ / /“)4 Providenc~ (b) Fm. 16.1
Page 624 and 625: 624 EXAMPLES OF RADAR SYSTEM DESIGN
Page 626 and 627: CHAPTER 16 MOVING-TARGET INDICATION
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628 MOVING-TARGET INDICATION [SEC,
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630 MOVING-TARGET INDICATION [SEC.
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632 MOVING TARGET INDICATION [SEC.
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. 646 MOVING- TARGET INDICATION [SE
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648 MOVING- TARGET lNDICA TION [SEC
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652 MOVING-TARGET INDICATION [SEC 1
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656 MOVING-TARGET INDICATION [SEC.1
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658 When o = Othe instead MOVING-TA
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662 MOVING TARGET INDICATION [SEC.1
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670 MO VINGTARGET INDICATION [SEC.
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672 MOVING TARGET INDICATION [SEC.1
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674 MOVING- TARGET INDICATION [SEC.
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676 MOVING-TARGET INDICATION ~SEC.
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CHAPTER 17 RADAR RELAY BY L. J. HAW
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682 RADAR RELAY [SEC. 172 transmitt
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684 RADAR RELAY [SEC. 17.3 staggeri
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686 RADAR RELAY [SEC. 17.4 excluded
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688 RADAR RELAY [SEC. 174 long sign
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h Video I 1 I Angle marks RADAR REL
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692 [SEC. 175 ḇ 1 1 1 I ~ LKal tr
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694 RADAR RELAY [SEC. 17.5 generato
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696 RADAR RELAY [SEC. 17.6 station
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698 RADAR RELAY [SEC. 17.6 Video si
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700 RADAR RELAY [SEC. 176 train. Th
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702 RADAR RELAY [SEC.17.7 be obtain
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704 RADAR RELAY @EC. 17.7 illustrat
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[11 1 Bas,c pulse I %e pulse i ~--.
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708 RADAR ltELA Y [SEC. 1743 wave f
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710 RADAR RELAY [SEC. 17.8 actual m
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. 712 RADAR RELAY [SEC. 17.9 Such a
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714 RADAR RELAY [SEC. 17.10 between
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716 RADAR RELAY [SEC. 17.10 signal
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718 RADAR RELAY [SEC. 17.11 suppres
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720 RADAR RELAY [SEC. 17.12 provide
Page 722 and 723:
722 RADAR RELAY [SEC. 17.13 relay l
Page 724 and 725:
724 RADAR RELAY [SEC. 17.14 TaLE 17
Page 726 and 727:
726 RADAR RELAY [SEC. 17.15 RADAR R
Page 728 and 729:
728 RADAR RELAY [SEC. 17.15 Modulat
Page 730 and 731:
730 RADAR RELAY [SEC. 17.15 the sec
Page 732 and 733:
732 RADAR RELAY [SEC. 17.10 pulses
Page 734 and 735:
734 RADAR RELAY [f+iEc.17.16 The vi
Page 737 and 738:
Index A Absorbent materials, 69 Abs
Page 739 and 740:
INDEX 739 B-scope, electrostatic, 5
Page 741 and 742:
INDEX 741 Fairbank, W. M.,80 F Fan
Page 743 and 744:
INDEX ’743 Microwave, reason for
Page 745 and 746:
INDEX 745 Radar, pulse,3 range perf
Page 747 and 748:
INDEX 747 Signal, interference of,
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Radar System Engineering

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