Yakovlev Yak-25
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The Yakovlev Yak-25 (NATO designation Flashlight) was a swept wing, turbojet-powered interceptor aircraft used by the Soviet Union.
[edit] Development
The Yak-25 originated from a need for long-range interceptors to protect the USSR's northern and eastern territory. The specification for a two-seat, twin-engine jet fighter and a related reconnaissance aircraft was issued by Stalin on 6 August 1951. The aircraft was to use the new Mikulin AM-5 turbojet. The first prototype, the Yak-120, flew on 19 June 1952.
The new design mounted the turbojets in pods in the wings, with bicycle landing gear, leaving the fuselage volume free for the two crewmen and a substantial fuel load, giving an unrefueled range (with external tank) of about 2,560 km (1,600 mi). The large, blunt nose contained the radome for the air-interception radar. Armament was two hard-hitting 37 mm NL-37L cannon with 50 rounds per gun.
Despite some significant problems the type was cleared for production in 1953. Early production models, designated Yak-25, were delivered the following year, although they were not yet to operational capacity thanks to problems with the 'Sokol' radar. As a result early aircraft used a modified version of the RP-1D (NATO 'High Fix') ranging radar instead. When the 'Sokol' (RP-6) was finally available, the newly equipped aircraft were designated Yak-25M, with deliveries starting in January 1955. The Yak-25M received a number of other improvements, including recoil dampers for the cannon, upgraded AM-5A engines (with the same thrust), and a slight increase in fuel capacity. It was first displayed at Tushino in July 1955, and received the NATO designation Flashlight.
The last Yak-25 interceptors were retired by 1967; the 'Mandrake' reconnaissance version soldiered on in various roles through the late 1970s. Like many other PVO interceptors of the Cold War era, the Yak-25M was not exported to the Warsaw Pact or other nations.
There was also another aircraft named Yak-25 - a light fighter prototype of 1947. After it lost a competition with MiG-15 and Lavochkin La-15, the first Yak-25 program was abandoned and the designation Yak-25 was re-used for a new interceptor. See Yakovlev Yak-25 (1947) for the description of that aircraft.
[edit] Variants
[edit] Interceptor variants
Some Yak-25M aircraft were later fitted with the 'Gorizont-1' system to allow them to be flown (via autopilot) by ground stations for ground control interception missions. These were redesignated Yak-25MG.
In 1955 and 1956 several Yak-25Ms were refitted as testbeds for air-to-air missile armament. The Yak-25K-5 carried 'Izumrud' radar and four RS-1U (NATO AA-1 'Alkali') beam-riding missiles on the wings inboard of the engine pods. The cannon were deleted. The Yak-25K-5 was used to test the K-75 missile, which did not enter service; the same was true of two Yak-25K-7L, with the abortive K-7 weapon. More promising was the Yak-25K-8, armed with two K-8 (NATO AA-3 'Anab') weapons, but this was terminated in favor of the upcoming Yak-28P.
[edit] Other variants
The reconnaissance derivative of the Yak-25, the Yak-25RV (Razvedchick Vysotnyj, "high-altitude reconnaissance"), was developed in 1957. It had a completely new, long-span straight wing of 23.4 meters (more than twice that of the Yak-25M interceptor) with a total area of 55 square meters. Camera and sensor packs were added in the fuselage. Some versions may have retained one cannon.
Despite its low wing loading, the 'Mandrake's' altitude performance was marginal at best, with considerable engine problems at high altitudes, excessive vibration, and primitive equipment that imposed high workloads for the crews. VVS nevertheless kept the Yak-25RV (NATO Mandrake) in service until 1974. A few were used in the late 1970s for monitoring of radioactive contamination, with specialized sensors; these were designated Yak-25RRV. Efforts in 1971 to develop the 'Mandrake' as a high-altitude interceptor (Yak-25PA) proved unsuccessful.
The derivative Yak-26 was developed as a bomber, but only nine were built. The Yak-27 was an upgraded version of the Yak-25 that added an auxiliary rocket engine for better high-altitude performance. The Yak-27V interceptor did not enter service, but more than 160 recce-optimized Yak-27R (NATO Mangrove) entered service in the late 1950s.
In 1961 a series of lightened 'Mandrakes' were produced as high-altitude target drones. The Yak-25RV-I was used as a manned target for unarmed (no live fire) interception practice, the Yak-25RV-II as a remote-piloted drone.
[edit] Users
[edit] Specifications (Yak-25)
General characteristics
- Crew: two
- Length: 15.67 m (51 ft 5 in)
- Wingspan: 10.94 m (35 ft 10 in)
- Height: 4.4 m (14 ft 5 in)
- Wing area: 28.94 m² (311.51 ft²)
- Empty weight: 5,675 kg (12,510 lb)
- Loaded weight: 8,675 kg (19,125 lb)
- Max takeoff weight: 9,450 kg (29,760 lb)
- Powerplant: 2× Mikulin AM-5 or Tumansky RD-9 turbojets, 23 kN (5,000 lbf) each
Performance
- Maximum speed: 1,090 km/h (680 mph)
- Range: 2,700 km with external tank (1,687 mi)
- Service ceiling: 15,200 m (50,000 ft)
- Rate of climb: 30 m/s (5,960 ft/min)
- Wing loading: 327 kg/m² (67 lb/ft²)
- Thrust/weight: 0.53
Armament
- Guns: 2× 37 mm Nudelman NL-37 cannon (50 rounds per gun)
[edit] Related content
Related development
Comparable aircraft
- Avro Canada CF-100
- Gloster Javelin
- F-89 Scorpion
- F-94 Starfire
- F-101 Voodoo
- Sud Aviation Vautour
- Sukhoi Su-9
