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词条 Mikoyan-Gurevich I-350
释义

  1. Design and development

  2. Operational history

  3. Specifications (I-350)

  4. See also

  5. References

  6. External links

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}}{{Infobox aircraft type

type= Experimental fighter aircraftnational origin= Soviet Unionmanufacturer= Mikoyan-Gurevichdesigner=first flight= 16 June 1951introduced=retired=status=primary user=more users= produced= number built= 2unit cost= developed from=variants with their own articles=developed into=
}}

The Mikoyan-Gurevich I-350 (Izdeliye M), was a Soviet Cold War-era experimental fighter aircraft. It was the first Soviet aircraft able to maintain supersonic speed.

Design and development

From 1947, work began on a new axial-flow turbojet by OKB-165, led by Arkhip Mikhailovich Lyulka. OKB Mikoyan-Guryevich designed the I-350 around this engine, the {{convert|46.107|kN|lbf|abbr=on}} Lyul'ka TR-3A (redesignated as the Lyulka AL-5). Resembling a scaled-up MiG-17, the I-350 had a long slim fuselage, mid-set 57° swept wings and a wide-chord fin mounting a tailplane at half-span.{{Citation needed|date=September 2015}}

Given the OKB designation Izdeliye M, it was the first Soviet fighter able to fly stably at supersonic speeds.[1] Redesignated as the I-350, the I-350M-1 first prototype was fitted with a RP-1 Izumrud airborne interception radar and the second prototype, I-350M-2, was fitted with a Korshun airborne interception radar.{{Citation needed|date=September 2015}}

Operational history

The I-350M-1 first flew on 16 June 1951, piloted by Grigoriy A. Sedov, but the engine failed shortly after takeoff, precipitating a hydraulic system failure. Despite battling very heavy control forces, the pilot made a successful landing after lowering the landing gear using the emergency undercarriage extension system. Four more test flights were made, with very poor engine reliability, before the I-350 programme was terminated in August 1951.[1]

Specifications (I-350)

{{Aircraft specifications
|plane or copter?=plane
|jet or prop?=jet
|ref=MiG: Fifty Years of Secret Aircraft Design,[2]Gunston[3]
|crew=1
|length main=16.652 m
|length alt=54 ft 8 in
|span main=9.73 m
|span alt=31 ft 11 in
|area main=36 m²
|area alt=390 ft²
|airfoil=
  • Root: TsAGI SR-12s
  • Tip: TsAGI SR-7s

|empty weight main=6,124 kg
|empty weight alt=13,501 lb
|loaded weight main=8,000 kg
|loaded weight alt=17,637 lb
|max takeoff weight main=8,710 kg
|max takeoff weight alt=19,202 lb


|see also=
|related=
|similar aircraft=

  • North American F-100 Super Sabre
  • Supermarine 545
  • Dassault Super Mystère B2

|lists=
}}

References

1. ^{{cite book |last=Gordon |first=Yefim |title=OKB Mikoyan |year=2009 |publisher=Midland |location=Hinkley |isbn=978-1-85780-307-5 |author2=Komissarov, Dmitry|page=131}}
2. ^{{cite book|last1=Belyakov,|first1=R.A.|last2=Marmain|first2=J.|title=MIG: Fifty Years of Secret Aircraft Design|date=1994|publisher=Naval Institute Press|location=Annapolis, Md.|isbn=978-1557505668|pages=163-164}}
3. ^{{cite book |last=Gunston |first=Bill |title=The Osprey Encyclopaedia of Russian Aircraft 1875–1995 |publisher=Osprey Publishing |location=London |year=1995 |edition=1st |isbn=978-1-85532-405-3|page=195}}

External links

{{commons category|Mikoyan-Gurevich}}{{Mikoyan aircraft}}

5 : Mikoyan aircraft|Soviet fighter aircraft 1940–1949|Abandoned military aircraft projects of the Soviet Union|Single-engined jet aircraft|Aircraft first flown in 1951

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