interceptor
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.
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 |
References and Credits:
- «Non-standard» MiGs , Aviation 1’1999;
- History and aircraft of Mikoyan design bureau / «Wings of Russia», 1999, CD-ROM /
- «Encyclopedia of armaments» / «Cyril & Mephodiy», 1998 – CD-ROM /
- «Artem Mikoyan» / M.Arlazorov, 1978 /
- «Vojenska letadla» / Vaclav Nemecek, Praha, 1982 /
- YE-152 / Russian Aviation Museum /