Light front-line fighter Su-37
first one with this name.
Light
front-line fighter jet of the OKB Sukhoi, a competitor of PRL
MiG .
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Article from the book
Ildar Bedretdinova "Su-25 and its modifications"
In January 1986 came the MIC decision to the Council of Ministers of
the USSR to create a new clock and all-weather versions of the
Su-25T - Su-25TM (factory designation T8-TM). But
work began were crossed with a promising new project C-37.
In 1989, pursuant to Resolution of the CPSU Central Committee and
USSR Council of Ministers on the machine-building plant named after
PO Dry was developed
conceptual design multipurpose fighter-bomber, who was awarded the
designation C-37. The
aircraft was intended to replace the park tactical strike aircraft
types: the Su-7, Su-17, Su-20, Su-22, Su-25 and MiG-21, MiG-23 and
MiG-27, located in the Air Force of the Soviet Union and set in the
Warsaw Pact, Yugoslavia, China, North Korea, Afghanistan, Peru. Finland,
India and others.
Based on studies of operational and tactical situation 90 years, it
was determined that the solution of problems in direct support of
ground troops should be tactical strike aircraft to a depth of 150
km, that is the area of the reserves of the first echelon. The
basis of the military doctrine of the 90's is an "air-ground
operation, which is a joint action of the Army and Air Force. In
this case, the Air Force should play a very active and sometimes
decisive role in achieving success.
The C-37 was designed for reconnaissance and hitting the ground
(surface) moving armored
and still small and area targets, military defense systems, day and
night and adverse weather conditions, and the destruction of shock,
transport aircraft and the confrontation with tactical and army
aviation the enemy, including the highly maneuverable combat
anti-tank helicopters and tactical aircraft.
Work on the design of airplane C-37 was conducted under the
leadership of VP Babak. Analysis
of tactical and technical requirements as well as the experience of
combat employment and operation of the Su-17 and Su-25 is taken into
account when forming the shape of the new aircraft.
In order to reduce time and cost for design, construction and
commercial production of C-37, provided for the installation of
systems, equipment and engine, designed and developed at that time.
Sensor-based sighting and navigation system were onboard
multifunction radar and opto-electronic system that allows us to
solve the aircraft combat missions during the day and night, and
adverse weather conditions.
The navigation system provided high precision aircraft entering the
goal. On an airplane
provided for the installation of a powerful electronic warfare
system designed for personal protection against weapons of radio and
infrared systems, guidance
and targeting anti-radar
missiles.
Aircraft weapon system included various types of air attack weapons,
both managed and unmanaged.
Draft Project C-37 was considered branch institutes of the MAP and
USSR Ministry of Defense and received a positive conclusion.
The questions about the possibility of mass production of aircraft
in one of the aircraft factories to the development of a feasibility
study. In addition,
explored the possibility of joint development and construction of
the aircraft with foreign partners. CB
ready to develop a working draft, but the prevailing political and
economic situation associated with the collapse of the Soviet Union,
not allowed to carry out this project.
However, work on the project C-37 is not in vain, and the chief
designer VP Babak set the
task to consider the use developments, obtained by projecting C-37
for the shock of the complex of the Su-25TM, work on which ran
parallel to the strong pace.
Features assigned to aircraft problems (a reliable overcoming enemy
air defense and effective combat use of weapons in the area of
finding the target), which differ significantly from the Su-25T, not
to mention the Su-25, which required the introduction of the
sighting and navigation system on-board multi-function radar
station, which, moreover, was to ensure the safe flight of aircraft
at low altitude with rounding terrain. Originally,
it was assumed the use of radar an 8-millimeter "Dagger" as a wall
container, development of the St. Petersburg Research Institute of
Radio Electronic Systems (NIIREK) NGOs Leninets. The
development team headed
by chief designer, MA Gramagin. Active
part in taking: deputy. Chief
Designer - BV Sukonin,
leading specialists VI Deep,
LA Drukker, DD Boxes
and other
At the enterprises of the holding company Leninets was manufactured
in August of prototypes radar "Dagger", intended for the state of
flight and laboratory tests. Flight
tests of several modes of radar "Dagger" were held in LII. MM Gromov
and landfill GK NII VVS, but due to the high financial costs
The first article about the Su-37 .
"AeroHobbi" № January 1992
The main purpose of the Su-37 - fighter-bomber capable of striking
at ground targets day and night in any weather, maintain a defensive
dogfight is far behind the front line. It
is also intended to act as an interceptor and reconnaissance
aircraft. Its high combat
effectiveness provided a completely new set of REO and weapons, as
well as a new approach to ensure the flight characteristics of the
aircraft and its survivability.
Though modern fighters are better suited for multi-use than previous
generations of aircraft, though their effectiveness in each role is
much lower than that of the specialized aircraft. So
today a superpower in the face of shrinking military budgets face a
choice between multi-purpose and highly specialized aircraft. Perhaps
the refusal of Americans from attack aircraft program stealth A-12
indicates that the balance is tilting in favor of multi-purpose
machines. If so, then the
Su-37 great future.
It is likely that the Su-37 will be developed by the USSR in
cooperation with the countries with less developed aviation
industry. This will allow
partners to obtain relatively inexpensive multi-purpose or special
(based on the Su-37) aircraft in accordance with their needs.
At the same time it can be assumed that the basic version of the
Su-37 for the Soviet air force would strike aircraft to replace the
Su-25. With increased by
40% take-off weight impact version of the Su-37 can carry 88% more
payload than a replacement aircraft. But
as the Su-25 is still responsible for their purpose, and the Soviet
Union is experiencing considerable difficulties, we should not
expect a change in the next 5-8 years.
The choice of parameters.
Designers Bureau named. Sukhoi
aircraft in its last use so-called concept of the three lifting
surfaces, but the Su-37 decided to apply the usual scheme of "duck". Selected
aerodynamic configuration is similar to those used in the modern
European fighter aircraft (Rafale, Eurofighter, "flu"). In
the aerodynamic configuration of the plane felt a noticeable
influence of his predecessor - the Su-27 interceptor, reflected in
the strong integration of the middle part of the fuselage with
well-developed wings.
Starting from the main purpose of the Su-37 as an attack aircraft
designed to fly near the ground in the area with heavy anti-aircraft
fire, it is surprising choice of single-engine power plant.From the
standpoint of survival increase the choice of two engines would be
preferable.
It is known that the Su-37 is accelerated from 600 to 1100 km / h at
an altitude of 1000 m for 14 s, and acceleration up to 1300 km / h
requires an additional 7.2 s, assuming its maximum speed at sea
level of approximately 1500 km / h come to the conclusion that the
aircraft will require propulsion system with a maximum thrust (in
afterburner mode) of about 180 kN. The
same number required thrust is obtained from the assumption that the
maneuverability of the Su-37, no worse than other modern
interceptors, as well as from its intended normal takeoff weight of
16-18 tons and a maximum of 25 tons Even the last American F-119
engine firm Pratt Whitney selected for fighter ATF, does not possess
such a high thrust, as nothing is yet known about the existence of
such an engine in the USSR. Required
value of thrust, although you can get the installation of two
engines. And yet, the
designers decided to leave the single-engine scheme.It gives the
right to assume that they are counting on the new engine, which is
found only in the development stage.
Geometric and aerodynamic characteristics of wing Su-37 were
estimated by successive approximations, based partly on incomplete
data and partly on the available power equations in the method of
similarity-wing Su-27.
Given the maximum speed of the Su-37 at sea level, and bearing in
mind that the drag due to the increased influence of end effect of
the wing should be slightly larger than the Su-27, we obtain the
wing area of about 45 m 2 . However,
this means that the overload 9g load on the wing will be about 3000
kg / m 2 ,
which is 10% higher than the similar parameter of the
Su-27.Therefore, the most probable area of the wing is equal to 50 m 2 . Wing
this area would provide a suitable unit load (500 kg / m 2 at
maximum takeoff weight and 360 kg / m 2 in
normal) and as a result of excellent maneuverability of a fighter.
Trump card
Development of complex electronic equipment Su-37 Soviet Union hopes
to overcome its backlog in this area from the Western developed
countries. As part of
navigating the complex Su-37 has a new radar, which, even under
severe electronic warfare provides:
-
overflight regime obstacle at low altitudes in the transonic
speed
-
ground attack ground and sea targets,
-
simultaneously tracking 10 targets
-
detection tracking and destroying low-flying targets at all
flight speeds as well as fixed targets, including those still
hanging from the helicopter, which is difficult to detect.
Optoelectronic system provides the use of aircraft at any time and
launch missiles with TV and laser guidance systems including ATGM.
Multi-channel infrared system (like the Western system FLIR) is
located in the container and ensures a missile with an infrared
remote control from 10 to 15 km. In
containers also housed equipment for the photo, infrared and
television intelligence. The
second trump card Su 37 of its weaponry. At
18 (!) Nodes external load the new Soviet aircraft capable of
carrying 8300 kg payload. This
is more than well-known American attack aircraft A-10. Except
for "Tornado", any modern fighter has a greater payload. Except
30 mm cannon aircraft is equipped with a wide nomenclature of
weaponry, including:
-
UR-class air surface, and special anti-radar missiles,
-
SD air to air short-and medium-range
-
ATGM to fight with armored targets,
-
NUR caliber 85-370 mm
-
free drop and guided bombs caliber up
to 1500 kg
-
Suspended containers with 30 mm cannons.
Providing combat survivability .
Much of the aircraft structure made to enhance its survivability. First
of all it concerns the reduction of tail-infrared signatures of
noise and partial use of stealth technology. The
presence of defensive weapons systems and application of new
technologies in the design enhances the active protection, making it
difficult to detect enemy aircraft.
In order to enhance passive defense fighter cockpit armored as well
as vital components of airframe engine fuel system. Tanks
are protected with polyurethane foam plastic prevent the explosion
and burning of fuel in contact with the projectile. The
total weight of passive protection exceeds 800 kg.
The ability to store a fighter on small plots (magnitude of the
folded wing 8,1 m) and the use of unpaved runways with the strength
of coverage 7-8 kg / cm 2 and
significantly increase the survivability of fighter aircraft in
combat.
Performance characteristics .
The high level of LTH Su-37 is the basis of ensuring the
effectiveness and survivability of the aircraft. Considerable
weight of the combat load, short takeoff and landing distances, the
possibility of basing on the damaged runway, and high
maneuverability make Su-37 is very effective attack aircraft.
Low specific fuel consumption provides a large range of aircraft
without refueling in flight, although the latter possibility is
provided at the request of representatives of the Bureau .P.O.Sukhoi.
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Su-37 - aircraft and the program
It's not about the Su-37, continuation "lines" of Su-27 fighter,
known to many specialists for flight demonstration on MAKS, but
about the Su-37, which, on a plan of the chief designer of the
aircraft V. Babak, was supposed to be a continuation of the the line
"tactical attack aircraft Su-25. He
never appeared on the show MAKS in his native homeland, but was
represented at the show in Dubai in 1991. It
was the first and last appearance of the project Su-37 "in public."
Considering this project from the standpoint of today's development
of tactical aircraft could be characterized as the Su-37 strike
fighter JSF, realized within the framework of military aviation
technology 4-th generation. The
reason for this is almost complete identity of a functional
"person", as well as many similarities and the technical concept of
the two aircraft.
The main purpose of the Su-37 was defeated heavily defended land
targets. To accomplish
this task aircraft armed with a wide nomenclature of weapons
air-to-surface missiles. The
total mass of payload, placed at 18 locations outside for good, was
8.5 m. At the same time the Su-37 was supposed to enforce and
destructive problems, both in the near-agile, and far missile
combat. This was to ensure the inclusion
of the weapons, in addition to SD "air-to-air short range and
built-in gun still and SD air-to-air medium-range missiles. Fairly
close to the JSF looked Su-37 and its flight and technical
characteristics. Both
aircraft had to have supersonic flight, but with a moderate value of
M (for JSF 1.6 and 1.8 for the Su-37) and without performing a
supersonic cruise flight. Both
aircraft had a normal takeoff weight of less than 20 tons (about 17
m for the JSF, and about 18 m for the Su-37) and were supplied with
one engine. When combat
load of about 4 tons estimated range of both aircraft exceeds 1000
km.
The only fundamental difference between the two planes in terms of
their technical appearance relates to the protection
of detection aircraft in combat. If
JSF high undetection should be ensured by
the integrated application of technology "stealth", then the Su-37,
this question was decided by the high combat survivability of
aircraft. Weight means to
ensure combat survivability was about 1.3 tons (more than 7% of
normal takeoff weight of aircraft).
Adopted by the above characterization of the Su-37 aircraft as the
JSF, is implemented in the framework of military aviation technology
4-th generation, is caused by identity, not only functional "face"
of aircraft. The identity
of the Su-37 and JSF are also seen in the overall technology
development of aircraft, especially the programs themselves create
these aircraft.
Except for the time required procedures (preparation of the CC CPSU
and the USSR Government), program development JSF aircraft and Su-37
are one "in spirit". As
well as the creation of the aircraft JSF, the development of the
Su-37 was commercial and from the outset
focused not only on the internal needs of the state but also to the
needs of foreign markets.
Broad market analysis conducted by the developers found that
potential buyers of the Su-37 on the external market may be 24
countries. By the time
the decision to build a prototype volume of pre-orders from other
countries amounted to 1000 units. (This
is the value of the same order as the export supply JSF program in
2000 units, adopted as a condition for the transition to full-scale
development aircraft). Only
the Chinese Air Force gave a preliminary order for 180 aircraft.
Interest of foreign customers in the prepared plane was the best
indicator of the prospects of a development project. This
interest contributed not only to the unique characteristics of a
functional "person" of the plane, but also assumes a relatively low
cost of the Su-37 on the market. According
to preliminary estimates, the price of the aircraft was not to
exceed $ 30 million (This is another of the same order as that of
the aircraft JSF, the price is a variant of the aircraft the Air
Force should be 28 million dollars).
A decision on the project was taken in 1990 All necessary
documentation is left to build on the serial works. Confidence
that the process has begun, "served as the basis for a broader and
more open advertising of aircraft development, which was used took
place in 1991, an international air show in Dubai. The
beginning was so encouraging that even the events of August 1991
were not originally perceived as relevant to the case. However,
the impact of these events - the collapse of the Soviet Union, the
elimination of Minaviaproma, termination of financing of works and
everything else made their own. Development
of the Su-37 was not only suspended but forgotten.Forgotten so that
the designation is assigned to the aircraft, "migrated" to another
development.And today, even an expert on the effectiveness of strike
aircraft, quickly discussing progress on JSF, can not remember the
first "Russian JSF".
It is hardly necessary to assume that the project Su-37, as they
say, ahead of his time. The
general decline of political and military tensions in the world,
which occurred in the late 80-ies not
without the active participation in the matter of domestic politics,
was accompanied (as it may seem strange to someone) reorientation of
tactical aviation to address shock problems. All
the European development of future combat aircraft (Eurofighter,
Rafale, Gripen) suddenly found non-compliant time and began to
urgently refined to meet shock problems. American
industry has not yet been drawn to this point in the program JSF,
responded to the urgent development of two attack fighter aircraft
based on existing aircraft 4-th generation. In
1987, the firm McDonnell Douglas began work on the development of
"lines" multipurpose aircraft F/A-18, and the firm General Dynamics
has finished in the early 90-ies before
the flight model development impact frontline aircraft A-16 on the
base of the supersonic Air Force F-16.
Development of the Su-37 fits into a similar course of development
of tactical aircraft, and could easily be implemented, if not for
the events mentioned above. The
implementation of the development of the Su-37 could provide, in
particular, and certain methodical effect in relation to the needs
of today. After a
large-scale commercialization of the product (which now takes place
in the PAK FA program, and many other programs to create new combat
aircraft) was originally planned as a major driving point in the
program of creation of the Su-37.
Vyacheslav Volodin, head of the SIC GosNIIAS
/ Journal of Air and Space № 6, 2001 /
Specifications
C-37
engine P-79 1 * 18143 kg
thrust-weight ratio 0.729 (max. take off.
weight)
length of 17.65 m
span 12.08 m / 8.64 m (folded)
Height 5.74 m
wing area 50 sq. m.
Wing loading 500 kg / m
Weight:
Max 24,970 kg
Normal 18000 kg
empty 12000 kg
Fuel 8300 kg (without PTB)
load 5000 kg - 8500 kg
Speed:
takeoff, landing 220 - 260 km / h
subsonic cruise
max. at high altitude
of 1500 km / h
ceiling of 17,000 m
range with normal combat load 5000 kg:
a land of 800 km
at high altitude 1500 km
maximum-load 9 / -3