Fighter Combat - Tactics and Maneuvering

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ONE-VERSUS-ONE MANEUVERING, SIMILAR AIRCRAFT 115 conventional aircraft generate turn-performance capability by maintaining speed within certain limits and by sacrificing altitude to gain a gravity assist, total energy (speed and altitude) must be considered in achieving a turn-performance advantage. Unless one fighter is able to generate a significant energy advantage, the usual loss of energy during the engagement often results in something resembling a slow-speed flat scissors or a stalemated nose-to-tail turn at tree-top level. I never went into the air thinking I would lose. Commander Randy "Duke" Cunningham, USN The Angles Fight The angles tactics outlined for the guns-only scenario are not as well suited for the RQ missiles case, but they maybe successful with minor modifications. Referring to Figure 3 -1, the angles fighter no longer has the threat of a gun snapshot at time "4" to force the bogey up, out-of-plane, in a nose-high move. This gives the bogey pilot freedom to continue a level or nose-low turn, leaving the angles fighter temporarily in an offensive, rearhemisphere position; but with an energy deficit, and probably a turnperformance disadvantage, the pilot of the angles fighter may have a difficult time improving on or maintaining his position. In such a case, the angles tactician might perform a low yo-yo after the overshoot to continue pressure on the bogey. Faced with an overshooting situation at time "4," it is likely that the bogey will attempt to capitalize by reversing nose-high, as shown in Figure 3-7. If so, the angles fighter pilot should pull sharply up to point at the ^C*jjg' R „ ^^ Figure 3-7. Angles Fight (RQ Missiles): Mid-Game
116 ONE-VERSUS-ONE MANEUVERING, SIMILAR AIRCRAFT bogey and threaten it as quickly as possible. If he is unable to point at the target and force it back down, the attacker should pull for a position behind and below the bogey, as shown at time "5." The angles fighter should climb as close to the bogey's altitude as possible at time "5," while retaining enough speed for maneuvering. The desired position at time "6" is slightly behind and beneath the bogey, with minimum nose-tail separation and the angles fighter's fuselage aligned as closely as possible with the bogey's. At time "6" both fighters will be near minimum-controllable airspeed. The angles fighter's position forces the pilot of the high fighter into a steeply banked turn, or a series of turn reversals similar to a flat scissors, in order to maintain sight of his opponent behind and below. The angles tactician should maneuver as necessary to remain out of sight on the bogey's belly-side. Concern over his opponent's position should eventually cause the bogey pilot to pull his aircraft's nose sharply down in order to increase his turn performance. Figure 3-8 depicts the end-game. After the bogey pilot has committed his nose steeply down, the angles fighter should continue a level turn until the bogey approaches co-altitude. At that point the pilot of the angles fighter can roll inverted and pull his nose sharply down toward vertical (time "7"). After overshooting the altitude of the angles fighter, the bogey pilot will usually begin a pull-out to increase AOT and maintain sight. If his turns are properly timed, the angles fighter pilot may be able to pull his nose to the target and fire (time Figure 3-8. Angles Fight (RQ Missiles): End-Game
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Fighter Combat TACTICS AND MANEUVER
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Preface ix Acknowledgments xv Abbre
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CONTENTS Vll Single-Side Offset 353
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X PREFACE tactics varied greatly, a
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Xll PREFACE current void of informa
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Acknowledgments Much of the credit
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Abbreviations AAA anti-aircraft art
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Fighter Combat TACTICS AND MANEUVER
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2 FIGHTER WEAPONS although fixed to
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4 FIGHTER WEAPONS some firing range
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Table 1-1. American Aircraft Guns T
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8 FIGHTER WEAPONS angle is also dep
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10 FIGHTER WEAPONS the ballistics o
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12 HGHTER WEAPONS often bars of lig
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14 FIGHTER WEAPONS This system has
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16 FIGHTER WEAPONS required firing
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18 FIGHTER WEAPONS With a disturbed
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20 FIGHTER WEAPONS We were both fly
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22 FIGHTER WEAPONS The predictor LC
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24 FIGHTER WEAPONS The next best th
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26 FIGHTER WEAPONS tracking G, shor
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28 FIGHTER WEAPONS defender's inten
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30 FIGHTER WEAPONS and acrobatic ma
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32 FIGHTER WEAPONS Missile Propulsi
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34 FIGHTER WEAPONS Missile Guidance
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36 FIGHTER WEAPONS straight path. T
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38 FIGHTER WEAPONS target to correc
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40 FIGHTER WEAPONS sensor systems,
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42 FIGHTER WEAPONS Since CW radars
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44 FIGHTER WEAPONS Missile Fuzes Th
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46 FIGHTER WEAPONS prised of many i
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48 FIGHTER WEAPONS The maneuvering
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50 FIGHTER WEAPONS racy being about
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52 FIGHTER WEAPONS then slowing the
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54 FIGHTER WEAPONS Shooter and targ
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56 FIGHTER WEAPONS will exhibit lar
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58 FIGHTER WEAPONS (RWR), that an e
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60 FIGHTER WEAPONS barrel-rolling a
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2 Basic Fighter Maneuvers I fly clo
Page 83 and 84: 64 BASIC FIGHTER MANEUVERS the comb
Page 85 and 86: 66 BASIC FIGHTER MANEUVERS himself
Page 87 and 88: 68 BASIC FIGHTER MANEUVERS speed ad
Page 89 and 90: 70 BASIC FIGHTER MANEUVERS pursuit
Page 91 and 92: 72 BASIC FIGHTER MANEUVERS Figure 2
Page 93 and 94: 74 Figure 2-7. Low Yo-Yo BASIC FIGH
Page 95 and 96: 76 BASIC FIGHTER MANEUVERS The pote
Page 99 and 100: 80 BASIC FIGHTER MANEUVERS In case
Page 101 and 102: 82 BASIC FIGHTER MANEUVERS capitali
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Page 111 and 112: 92 BASIC FIGHTER MANEUVERS subseque
Page 113 and 114: 94 Figure 2-22. Defensive Spiral BA
Page 115 and 116: 96 BASIC FIGHTER MANEUVERS usually
Page 117 and 118: 3 One-versus-One Maneuvering, Simil
Page 119 and 120: 100 ONE-VERSUS-ONE MANEUVERING, SIM
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Page 159 and 160: 140 ONE-VERSUS-ONE MANEUVERING, DIS
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166 ONE-VERSUS-ONE MANEUVERING, DIS
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1 70 ONE-VERSUS-ONE MANEUVERING, DI
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196 SECTION TACTICS, TWOVERSUS-ONE
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206 SECTION TACTICS. TWOVERSUS-ONE
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210 SECTION TACTICS, TWO-VERSUS-ONE
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226 SECTION TACTICS/ TWOVERSUS-ONE
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Section Tactics, Two-versus-Two The
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238 SECTION TACTICS, TWOVERSUS-TWO
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256 SECTION TACTICS, TWC-VERSUS-TWO
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7 Division Tactics The essence of l
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268 DIVISION TACTICS design began t
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270 DIVISION TACTICS so called beca
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272 DIVISION TACTICS "4." At time "
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274 DIVISION TACTICS Figure 7-8. Se
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276 DIVISION TACTICS Lieutenant Eug
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278 DIVISION TACTICS away, the free
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280 DIVISION TACTICS cloud) is now
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282 DIVISION TACTICS Figure 7-13. G
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284 DIVISION TACTICS defensive look
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286 DIVISION TACTICS In a dog-fight
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288 DIVISION TACTICS Americans empl
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8 Unlimited-Aircraft Tactics Of cou
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292 UNLIMITED-AIRCRAFT TACTICS seve
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294 UN LIMITED-AIRCRAFT TACTICS the
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296 UNLIMITED-AIRCRAFT TACTICS beca
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298 UNLIMITED-AIRCRAFT TACTICS I de
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300 UNLIMITED-AIRCRAFT TACTICS post
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302 UNLIMITED-AIRCRAFT TACTICS many
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304 UNLIMITED-AIRCRAFT TACTICS poss
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306 UNLIMITED-AIRCRAFT TACTICS posi
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308 UNLIMITED-AIRCRAFT TACTICS may
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310 UNLIMITED-AIRCRAFT TACTICS inte
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312 UNLIMITED-AIRCRAFT TACTICS A go
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314 UNLIMITED-AIRCRAFT TACTICS doct
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Fighter Missions To use a fighter a
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318 FIGHTER MISSIONS Scenarios Sinc
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320 FIGHTER MISSIONS altitude, deta
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322 FIGHTER MISSIONS agency and the
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324 FIGHTER MISSIONS As previously
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326 FIGHTER MISSIONS cruise missile
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328 FIGHTER MISSIONS pattern gives
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330 FIGHTER MISSIONS have to coordi
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332 FIGHTER MISSIONS can be turned
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334 FIGHTER MISSIONS the enemy. Suc
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336 FIGHTER MISSIONS aircraft, and
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338 FIGHTER MISSIONS point for a di
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340 FIGHTER MISSIONS become major t
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342 Figure 9-3. Fighter-Escort Miss
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344 FIGHTER MISSIONS Figure 9-6. Fi
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10 Tactical Intercepts Confront the
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348 TACTICAL INTERCEPTS Figure 10-1
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350 TACTICAL INTERCEPTS desired alt
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352 TACTICAL INTERCEPTS If the turn
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356 TACTICAL INTERCEPTS range). If
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358 TACTICAL INTERCEPTS ment, and t
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360 TACTICAL INTERCEPTS Advantages
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364 TACTICAL INTERCEPTS leader thro
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366 TACTICAL INTERCEPTS immediate l
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368 TACTICAL INTERCEPTS awareness),
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370 TACTICAL INTERCEPTS and positio
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372 TACTICAL INTERCEPTS low, traili
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376 TACTICAL INTERCEPTS also have t
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378 TACTICAL INTERCEPTS Visual Scan
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380 TACTICAL INTERCEPTS Likely thre
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382 TACTICAL INTERCEPTS be best for
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384 TACTICAL INTERCEPTS target on t
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Appendix Fighter Performance Perfor
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APPENDIX Figure A-l. V-n Diagram di
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APPENDIX 391 Figure A-2. Aircraft T
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APPENDIX 393 Figure A-4. Instantane
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APPENDIX 395 neuverability may be d
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APPENDIX 397 Figure A-7. Engine Thr
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APPENDIX 399 tends to reduce pressu
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APPENDIX 401 Figure A-11. Typical H
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APPENDIX 403 cause the Ps = 0 line
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APPENDIX 405 In theory the energy t
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APPENDIX 407 aircraft surfaces. In
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APPENDIX 409 Outside the zero-Ps li
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APPENDIX 411 factor," which is the
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APPENDIX 413 this condition occurs,
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APPENDIX 415 speed control. Many of
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APPENDIX 417 short or swept wings a
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420 BIBLIOGRAPHY Johnson, Robert S.
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422 INDEX Canard controls, 32, 398
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424 High yo-yo. See Yo-yo, high H-M
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426 INDEX Pursuit: curves and traje
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428 INDEX Turns (continued] 191, 20
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Fighter Combat - Tactics and Maneuvering

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