Practice fighter SU-25-UB
Designation
A practice fighter for 2-people crew is used for
training the crew to fly in favorable and
unfavorable meteorological conditions, at night
and by day and for helping the crew to master
the flight actions against the visible targets.
Typical enemies of the aircraft are as follows:
·
Tactical missiles and artillery at firing
positions, at marches and in the areas of
concentration
·
Tanks and motorized infantry in fighting or
pre-fighting or marching state, at the points of
support and in the areas of concentration
·
Management elements of infantry, army tactical
aviation
·
Army aviation helicopters (airplanes) on squares
and in the air
·
Fire sections and anti-aircraft means.
Tactical-technical characteristics
Crew |
2 men |
Geometric
characteristics |
|
Aircraft
dimensions: |
|
- Length,
m |
15,53 |
- Roll, m |
14,36 |
- Height,
m |
5,20 |
Net wing area, m2 |
30,10 |
Weight
specifications |
|
Weight of
an empty aircraft, kg |
10050 |
Takeoff
weight: |
|
- Normal,
kg |
15100 |
-
Maximum, kg |
18500 |
Landing
weight: |
|
- Normal,
kg |
11825 |
-
Maximum, kg |
13200 |
Maximum
military load, kg |
4000 |
Supply of
the fuel produced in internal tanks, l |
3430 |
Capacity of additional
fuel tanks
ПТБ-800
(4 pcs.), l |
820
each |
Capacity of additional
fuel tanks
ПТБ-1150
(2 pcs.), l |
1160
each |
Power
plant |
|
Type and
number of engines |
2 ТРД
Р-195 |
Emergency
traction force, kg.force |
2 х 4500 |
Flight-technical specifications |
|
Practical
roofing, m |
7000 |
Maximum
speed: |
|
- At the
ground, km/h |
940 |
- At
height, km/h |
М=0.82 |
Practical
range ability: |
|
- At the
ground, km/h |
495 |
- At
height, km/h |
1000 |
- From
4хПТБ-800, km |
1980 |
Takeoff
roll: |
|
- With
normal takeoff mass, m |
500 |
- With
maximum takeoff mass, m |
1050 |
Landing
roll: |
|
- With
normal landing mass, m |
550 |
- With
maximum landing mass, m |
750 |
Maximum
working load |
+6,5/-2,0 |
Armament |
|
Gun
armament: |
|
- Add-in
(integrated) gun device |
ВПУ-17А,
double-tube with 30-mm gun
ГШ-30,
supply of 250 bullets |
-
Demountable gun device (4 pcs.) |
СППУ-22-01,
double-tube
with 30-mm gun
ГШ-30,
supply of 260 bullets each |
Missiles
armament: |
|
-
Air-to-air guided missiles |
Р-60
(Р-60М) |
- Air-to-ground
(air-to-surface)
guided missiles |
Х-25
(Х-25МЛ), С-25Л, Х-29Л |
-
Unguided shells |
С-5, С-8,
С-13, С-24, С-25 |
Bomber
armament: |
|
- Aerial
bombs |
100, 250,
500 |
-
Incendiary
tanks |
ЗБ-500 |
-
Containers for small freights |
КМГУ-2 |
-
Single-mission bomb cartridges |
РБК-250,
РБК-500 |
Number of
suspension centers |
10 |
Briefly about the aircraft
The aircraft is a subsonic monoplane with low
height and for 2-person crew. Its active service
has been increased and its maneuvering
specifications are favorable at low speeds.
The aircraft may be exploited from concreted
runaway and airfields with frozen ground surface
cleaned off snow, as well as from the airfields
located in high mountains (at 3000 m above sea
level).
The cockpit is armored and is equipped with
conditioning and ventilation systems. The
cockpit is equipped with an oxygen caddy for the
pilot and an ejection seat.
The rear cockpit is equipped with a periscope to
improve the vision of the front hemisphere
during takeoff, landing and flight. The rear
cockpit of an instructor is additionally
equipped with a failure simulator of the
aviation instruments and systems in the front
cockpit and flight controls with the priority
action.
The radio equipment of the aircraft provides a
pilot’s communication to the overhead objects
and aircrafts in every range of operational
height and radius of the aircraft and transfer
of the identification signals. The aircraft is
equipped with short range and long range radio
navigation systems allowing flying and landing
at any time during the day and night, both in
favorable and unfavorable meteorological
conditions.
The sight system of the aircraft enables to
destroy the target in terms of visual vision.
The weapon control system may be used to prepare
and select the weapon and the mode of its
application, as well as to control explosives
and other elements of the aviation weapon in
terms of different loads of the aircraft.
A filming equipment and photo-control device
installed on the aircraft serve the purpose of
controlling the results of gun firing and
missile launch.
The aircraft safety system includes the
apparatus identifying the functioning radar
stations, automatic machine identifying passive
infrared defects and dipole scatterers.
The most important peculiarities of the aircraft
are:
·
Higher life cycle than that of the aircrafts of
front aviation at the expense of a complex of
special means
·
Powerful missile, bombing and artillery armament
·
Little time necessary for preparation for a
repeated flight, even in case the variant of
armament is changed
·
Relative simplicity of piloting techniques
·
High exploitation produceability of the aircraft
·
Capability of carrying out independent military
actions even from the ill-equipped airfield
·
High reliability of equipment, aggregates and
systems
·
Favorable vision from the pilot’s cockpit
·
The aircraft is equipped with higher-duty
engines with less IR radiation. |