Grumman F-14 Tomcat - Quiz
A) AIM-9 Sidewinder B) AIM-7 Sparrow C) AIM-54 Phoenix D) AIM-120 AMRAAM
A) Weapons Systems Officer B) Ground controller C) Radar Intercept Officer (RIO) D) Pilot
A) Rolls-Royce Pegasus B) Pratt & Whitney TF33 C) General Electric F101 D) General Electric F110-GE-400
A) F-14A B) F-14D C) F-14A+ D) F-14B
A) LANTIRN Targeting Pod B) Link 16 Datalink C) TARPS-DI D) Digital Flight Control System (DFCS)
A) F-14 Super Tomcat B) F-14C C) F-14A-Plus D) F-14A+
A) 1984 B) 1992 C) 1998 D) 2003
A) ROVER B) TARPS C) LANTIRN D) T3
A) Left engine intake B) Under the nose C) Centerline station D) Right wing glove pylon
A) TARPS-CD B) PTID C) ROVER III D) LANTIRN 40K
A) F-4 Phantom B) A-6 Intruder C) F/A-18 Hornet D) F-111B
A) Introduction of laser targeting B) Introduction of night vision C) Introduction of a digital camera D) Introduction of terrain following radar
A) AIM-9M B) AIM-54C C) GBU-38 JDAM D) AIM-7M
A) Only the navigation pod B) A custom three-pod configuration C) Only the targeting pod D) Both the navigation and targeting pods
A) Air defense operations B) Close air support C) Deep strike bombing D) Electronic warfare jamming
A) Mach 1.8 B) Mach 2.0 C) Mach 2.5 D) Mach 2.2
A) 25 mm GAU-12 Equalizer B) 20 mm M61 Vulcan C) 20 mm M39 D) 30 mm GAU-8 Avenger
A) Six B) Five C) Four D) Three
A) Variable-geometry B) Folding C) Swept-back D) Delta
A) Rockwell B) Grumman C) Vought D) Connolly
A) Wildcat B) Bearcat C) Hellcat D) Seacat
A) It was not a feline name B) Sexual connotations C) It was already taken D) It sounded too aggressive
A) January 1969 B) July 1968 C) December 1968 D) December 1970
A) F100 B) TF30 C) J79 D) F401-PW-400
A) 16,000 lb B) 12,000 lb C) 20,000 lb D) 18,000 lb
A) 6,000 hours B) 8,000 hours C) 7,200 hours D) 5,000 hours
A) 1975 B) 1970 C) 1972 D) 1973
A) 1990s B) 1970s C) 2000s D) 1980s
A) December 1970 B) April 1972 C) April 1973 D) January 1969
A) 80 nmi B) 150 nmi C) 110 nmi D) 100 nmi
A) Six B) Four C) Ten D) Five
A) 100% B) 75% C) 80% D) 66%
A) 21 December 1969 B) 1 January 1969 C) 21 December 1970 D) 21 December 1973
A) F-15 Eagle B) F-111 Aardvark C) F-4 Phantom II D) F-16 Fighting Falcon
A) Naval Fighter Experimental (VFX) B) Fleet Air Defense (FAD) C) VFAX D) Tactical Fighter Experimental (TFX)
A) McDonnell Douglas F-4 Phantom II B) Douglas F6D Missileer C) Boeing F/A-18E/F Super Hornet D) General Dynamics F-111B
A) Electronic warfare B) Aerial refueling C) Precision ground-attack missions D) Long-range interception
A) 1 January 2005 B) 22 September 2006 C) 22 September 2000 D) 21 December 1970
A) General Dynamics F-111B B) Douglas F6D Missileer C) Boeing F/A-18E/F Super Hornet D) McDonnell Douglas F-4 Phantom II
A) Soviet Union B) Iran C) Vietnam D) Iraq
A) It was renamed to the F-14 B) It was canceled C) It was used in the Vietnam War D) It entered service in 1959
A) Shah Mohammad Reza Pahlavi B) Thomas F. Connolly C) General Dynamics D) Robert McNamara
A) Boeing B) Douglas C) Grumman D) McDonnell Douglas
A) FAD-1 B) Model 303 C) VFX-1 D) TFX-2
A) Failure to carrier landing B) Difficulty going supersonic C) Excessive fuel consumption D) Too much maneuverability
A) At least 160 B) 55 C) 16 D) 100
A) Twin-engine B) Single-seat C) Supersonic D) Twin-tail
A) A-12 Avenger II B) VFMX C) F/A-18E/F Super Hornet D) NATF
A) A-12 B) A-6 C) F-22 D) F/A-18
A) 1988 B) 1993 C) 1991 D) 1989
A) 2015 B) 2010 C) 1995 D) 2000
A) 55 B) 18 C) 37 D) 132
A) Donald Rumsfeld B) Robert McNamara C) Caspar Weinberger D) Dick Cheney
A) Engine thrust upgrade B) Radar range extension C) AIM-120 AMRAAM capability D) Stealth coating application
A) 1950s technology B) 1970s technology C) Outdated Cold War technology D) 1960s technology
A) 100 B) 55 C) 132 D) 80
A) National security asset B) Jobs program C) Technological failure D) Expensive relic
A) 1989 Defense Review B) 1993 Bottom-Up Review C) 1991 Procurement Review D) 1995 Strategic Review
A) Lockheed Corporation B) Northrop Corporation C) General Dynamics D) Boeing
A) Two-seat cockpit with a bubble canopy B) Side-by-side cockpit C) Tandem three-seat cockpit D) Single-seat cockpit with a flat canopy
A) T-tail empennage B) Single vertical stabilizer C) V-tail empennage D) Twin-tail empennage
A) In the center of the fuselage B) On the left side C) On the right side D) Under the nose
A) 10 to 20 percent B) 40 to 60 percent C) 70 to 80 percent D) 5 to 10 percent
A) To support heavy ground bombs B) To handle high-speed taxiing C) To allow for off-road landings D) To withstand carrier catapult launches and recoveries
A) Folding wing motors only B) Fuel, avionics, and weaponry C) Crew sleeping quarters D) Extra jet engines
A) Stacked vertically on top of each other B) In widely spaced nacelles C) Deep inside the main fuselage D) Within the wings
A) 55 degrees B) 68 degrees C) 75 degrees D) 80 degrees
A) Electron beam welding B) Cold forging C) Aluminum riveting D) Laser cutting
A) They double their effectiveness B) They are disabled C) They function as air brakes D) They lock in the neutral position
A) 7 degrees B) 17 degrees C) 35 degrees D) 10 degrees
A) 17 degrees B) 10 degrees C) 7 degrees D) 35 degrees
A) The tailhook B) The fuel dump valve C) The drag chute D) The auxiliary power unit exhaust
A) Pratt & Whitney F401 B) General Electric F110-GE-400 C) Pratt & Whitney F100 D) Pratt & Whitney TF30-P-412A
A) General Electric F100 B) Pratt & Whitney TF30-P-414A C) General Electric F110-GE-400 D) Pratt & Whitney F401
A) 28% B) 40% C) 10% D) 15%
A) Oil pressure loss B) Fuel leakage C) Overheating D) Compressor stalls
A) Unrecoverable flat spin B) Engine explosion C) Immediate flameout D) Loss of all electrical power
A) Structural stress on the catapult B) Engine failure could cause uncorrectable yawing moments C) Excessive engine heat damage D) High fuel consumption
A) Decreased by 10% B) Increased by 61% C) Increased by 25% D) Increased by 100%
A) The engine intake became blocked by debris B) The bleed air pressure dropped too low C) Exhaust gases could cause compressor stalls D) The vibration damaged the engine bay
A) 0.85 B) 0.73 C) 0.95 D) 0.56
A) Martin-Baker GRU-7A B) Boeing ACES II C) Martin-Baker GRU-5B D) Lockheed Martin E-1
A) Garrett AiResearch B) General Electric C) Hughes Aircraft D) Northrop Grumman
A) Raytheon AN/APG-65 B) Hughes AN/AWG-9 C) Westinghouse AN/APG-66 D) Northrop APG-71
A) 36 B) 12 C) 24 D) 6
A) APG-71 B) AN/APG-63 C) AN/APG-73 D) AN/AWG-10
A) Tactical Control System B) TV Set C) Target Capture Sensor D) Thermal Calibration System
A) Gallium nitride semiconductors B) MOSFET-based large-scale integration C) Vacuum tube vacuum arrays D) Bipolar junction transistor modules
A) Silicon carbide B) Cadmium telluride C) Gallium arsenide D) Indium antimonide
A) Six B) Two C) Four D) Three
A) AN/AAS-42 B) AAX-2 C) AN/ALR-67 D) AN/AWG-11
A) 450 knots B) 550 knots C) 300 knots D) 600 knots
A) AN/ALR-45 B) AN/ALR-50 C) AN/ALR-23 D) AN/ALR-67
A) Japanese long-range bombers B) Soviet anti-ship cruise missiles C) Chinese reconnaissance drones D) German jet fighters
A) Attack-F14 B) Ground-Cat C) Strike-Tom D) Bombcat
A) Five times B) Twice C) Zero times D) Once
A) The missiles hit the wrong targets B) The rocket motors did not ignite C) The pilot accidentally jettisoned the missiles D) The missiles scored two kills
A) The missiles were improperly armed B) Enemy jamming prevented a lock C) The radar malfunctioned D) The pilot forgot to turn on the master arm
A) R-77 Adder B) R-73 Archer C) R-60 Aphid D) R-27R Alamo
A) Project Sky Hawk B) Project Hawk Eye C) Project Persian Tomcat D) Project Desert Shield |
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