https://www.horizonhobby.com/f-4-phantom-ii-80mm-edf-bnf-basic-with-as3x-safe-select-efl7950
McDonnell Douglas F-4 Phantom II
(Wikipedia)
- On 6 June 1971, Hughes Airwest Flight 706, a McDonnell Douglas DC-9-31 collided in mid-air with a United States Marine Corps F-4B Phantom above the San Gabriel Mountains, while en route from Los Angeles International Airport to Salt Lake City. All 49 on board the DC-9 were killed, while the pilot of the F-4B was unable to eject and died when the aircraft crashed shortly afterwards. The F-4B's Radar Intercept Officer successfully ejected from the plane and parachuted to safety, being the sole survivor of the incident.
- On 9 August 1974, a Royal Air ForcePhantom FGR2 was involved in a fatal collision with a civilian PA-25-235 Pawneecrop-sprayer over Norfolk, England.
- On 21 March 1987, Captain Dean Paul Martin (son of entertainer Dean Martin), a pilot in the 163d Tactical Fighter Group of the California Air National Guard, crashed his F-4C into San Gorgonio Mountain, California shortly after departure from March AFB. Both Martin and his weapon systems officer (WSO) Captain Ramon Ortiz were killed.[177]
- Data from The Great Book of Fighters[104] Quest for Performance,[18] Encyclopedia of USAF Aircraft,[52]and McDonnell F-4 Phantom: Spirit in the Skies[178]General characteristics
- Crew: 2
- Length: 63 ft 0 in (19.2 m)
- Wingspan: 38 ft 5 in (11.7 m)
- Height: 16 ft 5 in (5 m)
- Wing area: 530 sq ft (49.2 m2)
- Aspect ratio: 2.77
- Airfoil: NACA 0006.4–64 root, NACA 0003-64 tip
- Empty weight: 30,328 lb (13,757 kg)
- Gross weight: 41,500 lb (18,824 kg)
- Max takeoff weight: 61,795 lb (28,030 kg)
- Maximum landing weight: 36,831 lb (16,706 kg)
- Fuel capacity: 1,994 US gal (1,660 imp gal; 7,550 l) internal, 3,335 US gal (2,777 imp gal; 12,620 l) with 2x 370 US gal (310 imp gal; 1,400 l) external tanks on the outer wing hardpoints and either a 600 or 610 US gal (500 or 510 imp gal; 2,300 or 2,300 l) tank for the centre-line station.
- Powerplant: 2 × General Electric J79-GE-17A after-burning turbojet engines, 11,905 lbf (52.96 kN) thrust each dry, 17,845 lbf (79.38 kN) with afterburner
- Maximum speed: 1,280 kn; 1,473 mph (2,370 km/h) at 40,000 ft (12,000 m)
- Maximum speed: Mach 2.23
- Cruise speed: 508 kn; 584 mph (940 km/h)
- Combat range: 367 nmi; 423 mi (680 km)
- Ferry range: 1,457 nmi; 1,677 mi (2,699 km)
- Service ceiling: 60,000 ft (18,000 m)
- Rate of climb: 41,300 ft/min (210 m/s)
- Lift-to-drag: 8.58
- Wing loading: 78 lb/sq ft (380 kg/m2)
- Thrust/weight: 0.86 lbf/lb (0.0084 kN/kg) at loaded weight, 0.58 lbf/lb (0.0057 kN/kg) at MTOW
- Takeoff roll: 4,490 ft (1,370 m) at 53,814 lb (24,410 kg)
- Landing roll: 3,680 ft (1,120 m) at 36,831 lb (16,706 kg)
- Armament
Performance
▪(Wikipedia)
KJV
https://kimchirev12.blogspot.com/2018/11/revelation-12- prophecy-trail-onthe.html?m=1
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