Mikoyan/Gurevich Ye-152A
1959
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Mikoyan/Gurevich Ye-152A

For high speed development purposes and as a test bed for a 15-tonne engine that was being developed by the Tumansky bureau with a view to powering a proposed Mach=3.0 high-altitude interceptor (which was to materialise as the MiG-25), the MiG OKB developed what was ostensibly a pure research aircraft, the Ye-150. Powered by a Tumansky R-15-300 engine of 6840kg boosted to 10150kg with afterburning, the Ye-150 flew for the first time on 8 July 1960, and was subsequently to attain a speed of Mach=2.65 or 2816km/h and a ceiling of 22500m. Design of an all-weather high-altitude interceptor based on the research aircraft had paralleled work on the Ye-150. As the Ye-152A, this had been adapted to take two thoroughly proven R-11F-300 engines owing to development problems with the large R-15 engine which were resulting in serious delays. In consequence, the Ye-152A interceptor fighter was ready to fly before the Ye-150 research aircraft upon which it was based, this event taking place on 10 July 1959. Powered by two R-11F-300 engines each rated at 3900kg and 5740kg with afterburning, the Ye-152A was intended to carry the Uragan 5B radar accommodated in a large, fixed intake centrebody and a pair of MiG-developed K-9 (K-155) long-range beam-riding missiles. While the intake centrebody of the Ye-152A was non-translatable, the extreme forward fuselage with intake orifice was hydraulically movable, thus achieving the same effect as a fully-variable shock cone. The Ye-152A was overtaken by the R-15-powered Ye-152, and its flight test programme was terminated after 55 flights of which only two were made carrying K-9 AAMs.

3-View 
Mikoyan/Gurevich Ye-152AA three-view drawing (1657 x 977)


Specification 
 WEIGHTS
    Take-off weight13960 kg30777 lb
 DIMENSIONS
    Wingspan8.49 m27 ft 10 in
    Length19.00 m62 ft 4 in
    Wing area34.02 m2366.19 sq ft
 PERFORMANCE
    Max. speed2500 km/h1553 mph
    Ceiling19800 m64950 ft

Comments 
Pater, 13.11.2008

First F-14's suffered from US-capitalist-made engines "self-destruction". Two of them were destroyed at laughable speed of M=0,5, pretty far from Soviet-build engines' "redline"...
Keep on trying, branwashed wannabe-a-doctor.

Dr. Nick Stage phd., sarge_46077(@)yahoo.com, 26.05.2008

This aircraft, an "actively-deployed-prototype"
was wrongly-called, by N.A.T.O., in 1964-through-1967,
the "MIG-23" and the "FLIPPER", and was flown to
MACH 2.94, before the Soviet-built Tumansky-266-305 exploded, killing the pilot and destroying this plane.
This tragedy occured on December 15th, 1966.
After this, any Soviet Mig or Soviet Sukhoi aircraft had
"red-line" limits on speed, engine duration, structural
integrity,turning-capability and altitude-sustainablity.
Even the new SU-37 "Super-Flanker", also called
"the Terminator-B" can only go at Mach-3.4--only in a dive.
The new U.S. F-22 fighter-jet, and the new U.S. F-15K ,
would be able the "kill" the SU-37 by a theoritical
air-combat "kill-ratio" of 22-to-1.

These same Tumansky jet engines were used, after some
modifications, in the twin-engined Soviet MIG-25 "Foxbat" interceptor.

MIG-25 pilots could use these same engines, later
called the Tumansky R-15G-2 engine,
lacked advanced analog-control, so the Mig-25 was limited
to no more than 375 miles--in radius, and the aircraft
was "red-lined" at Mach 2.8-to-3.0.
Above this speed, the R-15 engines went into ramjet-mode,
but after 5-to-8 minutes, these engines were totally
wrecked, and to be entirely replaced.

This information came from Captain Viktor Belenko,
on his defection from Vladivostol and landing
in Japan, and surrendering his Mig-25, early
September of 1976.
Just as Captain Belenko's Mig-25 was "touching down",
the aircraft completely ran out of fuel--guaranteeing
one heck of a VERY HARD landing.
The MIG-25's "sink-rate" was as bad a the U.S. Space
Shuttle which has only a ONE CHANCE-only landing
approach.

To return to YE-152A:
For the late 1960's or even the early 1970's, this
aircraft would have been a "sky-killing" jet, especially
in the INTERCEPTOR role, but like the MIG-25, the
G-loads of 4 or 5 G's, would have enough to have
had this otherwise good aircraft to structural failure.

The Soviets did this best they could with the crude
building techniques, like using heavy steel, and very
heavy nickel-plated stainless steel engines.

Keep em' flying--smilin' Ivan!!

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