Krastenfeld K4 Sturmvogel

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Krastenfeld K4 Sturmvogel
Krastenfeld K4.png
Preserved Englean K4-H7, 2015
Role Interceptor, fighter-bomber
National origin Englean Empire
Manufacturer Krastenfeld Luftschiff- und Flugzeugbau
Designer Erik Geberson
First flight 1958
Introduction 1960
Retired 1999 (Englean Empire)
Status In limited service
Primary users Luftstreitkräfte (historically)
Aruschan Republican Air Force
Produced 1958-1983
Number built 5,875

The Krastenfeld K4 Sturmvogel is a tandem two-seat, twin-engine, all-weather, long-range supersonic jet interceptor and fighter-bomber originally developed for the Englean Luftstreitkräfte but later was exported and used by various air forces around the globe. The vehicle was a resiliant and effective aircraft, being adapted for multiple roles outside of its designated interceptor and fighter-bomber roles. With a top speed over mach 2.2, the K4 became the Luftstreitkräfte's primary air-superiority fighter through the majority of the Cold War.

The K4 was used within various wars during the period between 1960 and 1999, becoming a well-known aircraft in many militaries around the world. It was notable in Ventismar for its ability to act as a counterpart for the Libriran Pa-100 "Sickle" and as a deterrant for Libriran strategic bombers. The Luftstreitkräfte briefly armed the K4 with nuclear weapons from 1968 to 1978, when it was decided that the tactic of the deployment of tactical nuclear weapons was becoming obsolete.

The K4 was retired by the Luftstreitkräfte in 1999, but remains in service with many nations within Sunalaya.


Operators


Specifications

3-side view of the F-4E/F

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: ESA 345-20 root, ESA 345-23 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 center-line station.
  • Powerplant: 2 × Imperial Electric and Motor Works IEW-3984 after-burning turbojet engines, 11,905 lbf (52.96 kN) thrust each dry, 17,845 lbf (79.38 kN) with afterburner

Performance

  • Maximum speed: 1,280 kn; 1,473 mph (2,370 km/h) at 40,000 ft (12,000 m)
  • Maximum speed: Mach 2.25
  • 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 at loaded weight, 0.58 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