词条 | Lavochkin La-250 | ||||||||||||||||
释义 |
The Lavochkin La-250 "Anakonda" was a high-altitude interceptor aircraft prototype developed in the Soviet Union in the 1950s. Its nickname "Anaconda" was invented during the flight test and referred to both the elongated body shape as well as the relatively critical flight characteristics of the machine. DevelopmentBy the mid-1950s, it became obvious that subsonic cannon-armed fighters such as the Yakovlev Yak-25 would be unable to intercept fast high-altitude targets like the upcoming generation of strategic jet bombers. As a result, in 1953 Lavochkin OKB proposed addition of an air-to-air missile system to the Berkut air-defense system. Tasked with defense of Moscow, the Berkut system consisted of a large network of radars and surface-to-air missile sites as well as ground-controlled interceptor aircraft. Lavochkin's proposed missile, the G-300 utilized a guidance system based on vacuum tubes and was so heavy (about 1,000 kg (2,200 lb)) that no fighter in the Soviet arsenal could carry it. Instead, a Tupolev Tu-4 bomber (Soviet version of the Boeing B-29 Superfortress) was modified to carry four G-300s under the wings, with the whole system receiving designation G-310. For all this trouble, G-300 was expected to have a range of only {{convert|15|km|mi}} and a ceiling of {{convert|20,000|m|ft}}. Although G-310 made ten flights in 1952, the system was abandoned as impractical. In November 1952, the Soviet government ordered development of Kompleks K-15 (Complex K-15, a notion analogous to USAF's "weapon system" concept). K-15 was to consist of an "interceptor 250" (later designated La-250) carrying "Type 275" guided missiles. La-250 had to be able to intercept targets flying at {{convert|1250|km/h|mph|abbr=on}}, Mach 1.18) at {{convert|20000|m|ft}} up to {{convert|500|km|mi}} from the airbase. Initial guidance was to be from Vozdukh-1 ground control with terminal onboard radar guidance for the last {{convert|40|km|mi}} and automatic missile firing by the fire control system when in range. Missile "275" was projected to weigh {{convert|870|kg|lb}} and, powered by a liquid fuel rocket motor, its top speed was to exceed {{convert|3900|km/h|mph|abbr=on}}. With a {{convert|125|kg|lb}} conventional warhead, it had a projected lethal radius of {{convert|50|m|ft}}. La-250 was to carry two "275" missiles semi-recessed into the underside of the fuselage in a tandem arrangement. The first flight took place on 16 July 1956 by Andrei G. Kochetkov. Problems with the K-15U radar and Klimov VK-9 engines forced a radical redesign of the aircraft to use the K-15M radar and, more importantly, much less powerful Lyulka AL-7F engines. This, in turn, led to the need to change "275" missiles to the lighter "275A" (although total missile weight decreased to {{convert|800|kg|lb}}, the warhead actually grew to {{convert|140|kg|lb}}. The new airframe with a smaller fuselage and a delta wing instead of the earlier swept wing was designated La-250A. The "275" missiles were now carried on underwing pylons. The lighter airframe was not enough to overcome the weaker engines, and projected performance suffered compared to La-250. While busy redesigning the aircraft, Lavochkin OKB also had to develop new variants of the "275" missile - the semi-active radar homing "277," the nuclear-armed "279," and solid fuel rocket-powered "280." The first La-250A prototype was finally rolled out on 16 June, 1956. Test flights of the five prototypes were plagued by crashes caused by failures of the hydraulic boost system and landing gear as well as poor forward visibility (the latter was corrected with fitting of a new slightly "drooped" nose). La-250A made a single test flight in 1956, only 6 flights in 1957, and a mere 14 flights in 1958. Frustrated by the lack of progress, Soviet Air Force stopped all work on the K-15 system in 1959. Lessons learned with K-15 were used to develop new interceptor system requirements which led to the Tupolev Tu-28 interceptor. The abortive, trouble-filled development of La-250 was mirrored in the West by the similarly complicated creation of Convair's delta-winged F-102 Delta Dagger and F-106 Delta Dart interceptors, which however eventually resulted in operational weapon systems. SurvivorsOne of Lavochkin La-250A prototypes is on display at the Central Air Force Museum at Monino, outside of Moscow, Russia.[1] Specifications (La-250A){{aircraft specifications||plane or copter?=plane |jet or prop?=jet |crew=2 |length main=26.80 m |length alt=87 ft 11 in |span main=13.90 m |span alt=45 ft 7 in |height main=6.50 m |height alt=21 ft 4 in |area main=80.0 m² |area alt=860.8 ft² |empty weight main=18,988 kg |empty weight alt=41,775 lb |loaded weight main=24,500 kg |loaded weight alt=53,900 lb |max takeoff weight main=27,500 kg |max takeoff weight alt=60,500 lb |engine (jet)=Lyulka AL-7F |type of jet=turbojets |number of jets=2 |thrust main=98.0 kN |thrust alt=22,050 lbf |thrust more=afterburning thrust |max speed main=1,800 km/h (1,118 mph) without missiles; 1,600 km/h |max speed alt=994 mph |max speed more=with missiles |range main=2,000 km |range alt=1,240 mi |ceiling main=17,000 m |ceiling alt=55,760 ft |loading main=306 kg/m² |loading alt=63 lb/ft² |thrust/weight=0.41 |more performance= |armament=
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1. ^ Monino home page {{Lavochkin aircraft}} 7 : Lavochkin aircraft|Abandoned military aircraft projects of the Soviet Union|Soviet fighter aircraft 1950–1959|Twinjets|Delta-wing aircraft|Mid-wing aircraft|Aircraft first flown in 1956 |
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