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Е-152А «Flipper»
interceptor

E-152A

    In June 1959 E-152 aircraft was built and presented for production flight tests.
    The Mikoyan Design bureau pioneered the use of honeycomb fillers increasing stiffness and reducing by 10-18% weight of stabiliser, ailerons and flaps. The first E-152A flight was made on July 10, 1959; aircraft was flown by test pilot G.K.Mosolov. Flights to assess stability and manoeuvrability characteristics, and determine aircraft performance have been made during the last six months of 1959. Development of K-9 armament system forming part of «Uragan-5» complex was not carried out, since same units of ZP-1 radar and AZO-SPK equipment were not delivered for tests.Flight E-152A on Tushino
    The second E-152A prototype was under construction till October 1959; later it was used to build the second E-152 prototype powered by R-15-300 engine.
    Upon completion of flight test program in August 1960, E-152-9 intercept equipment was installed on E-152A aircraft in place of «Uragan-5» system. E-152-9 complex consisted of: interceptor-fighter, armament system including ZP-1 radar and K-9 guided rockets with their control devices, VB-158 computer, SAZO-SPK «Meteorit» system for command and active response transmission, AP-39 autopilot, KSI compass system, «Put-2» flight instrument set and other equipment. Flight tests of individual components (ZP-1 radar, AP-39 autopilot, VB-158 computer, K-9 rockets) began by the late 1961. A short time later, the aircraft equipped with launchers for K-9 guided rockets was transferred to GK NII VVS, where it continued tests, made 39 flights and 10 rocket firing.
     E-152A aircraft participated at Tushino air parade on July 9, 1961. In NATO it has received the code name Flipper for the extended form of a tail part with the large ventral strakes.
    The Mikoyan Design bureau could not begin tests of individual components for a new E-155 interceptor-fighter using E-152M aircraft, since R-15B-300 engines were not delivered in 1962-1965. The plant had to use E-152A aircraft for these tests. On January 29,1965, E-152A crashed performing the test flight. Test pilot I.N.Kravtsov died.
    The documentation on E-152A (without engines, rockets and radar) was transferred to China, which used it at creation of a fighter - interceptor J-8.

Description
Design OKB A.I.Mikoyan
Type E-152A
NATO designation Flipper
Year 1959
Function all-weather interceptor
Crew 1
Dimensions & Weight
Length, m 19 (18,61)
Wing Span, m 8,488
Wing Area, m2 32,02
Overall height, m 5

Take-off weight, kg        

13550 (12720)
Internal fuel, kg 3560
Power-plant
Engines 2 Turbojet R-11F-300
Thrust, kgf (kN) max 3880
in afterburner 5740
Flight data
Max. speed at altitude 13,7 km, km/h (M=) 2135 (1,99)
Landing speed, km/h 287
Practical ceiling, m 19800
Max g-load 7
Range, km 2300
Time to climb, min 10000 m 1,48
20000 m 7,64
Take-off run (with missiles), m 1000 (1295)
Landing run, m 1600

Armament

Missiles 2 K-9-155

Scheme E-152A

E-152A

References and Credits:

  1. «Non-standard» MiGs , Aviation 1'1999;
  2. History and aircraft of Mikoyan design bureau / «Wings of Russia», 1999, CD-ROM /
  3. «Encyclopedia of armaments» / «Cyril & Mephodiy», 1998 - CD-ROM /
  4. «Artem Mikoyan» / M.Arlazorov, 1978 /
  5. «Vojenska letadla» / Vaclav Nemecek, Praha, 1982 /
  6. YE-152 / Russian Aviation Museum /

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