GENERAL   EQUIPMENT   INC.                    

 

8724 Sunset Drive #191 Miami FL 33173 USA                                  

                                                  
Email:
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SUKHOI SU-25

 

 

TYPE:

Aircraft

DESCRIPTION:

Reconditioned Sukhoi SU-25K and SU-25 UB

PRICE:

Upon Request

PACKING:

Ex-works

 

 

RECONDITIONED SUKHOI SU-25K & SU-25UB (FROGFOOT)

 

 

 

 

 

Name: Frogfoot Su-25K
Manufacturer: Sukhoi (Russia)

Frogfoot Background

 

Dimensions

Wing Span: 47.11 ft. / 14.36 M
Length: 50.95 ft. / 15.53 M
Height: 15.75 ft. / 4.80 M
Wing Area: 362.74 Sq ft. / 33.70 Sq M
Aspect Ratio: ---
Weight Empty: 20,944 lb. / 9,500 Kg
Weight Takeoff: ---
Max. Takeoff Weight: 45,195 lb. / 20,500 Kg

Power & Performance

Powerplant(s): 2x Soyuz/Tumanski R-195 turbojet
Max Thrust: 9,920 lb.
Military Thrust: 9,920 lb.
Internal Fuel: ---
Fuel Fraction: ---

Max. Thrust Loading: 0.44
Combat Thrust/Weight Loading: ---

Maximum Wing Loading: 124.59 lb. per Sq. ft.; 608.31 Kg / Sq. M
Combat Weight Wing Loading: ---

VMax High Altitude / VMax Low Altitude: -- / --
Max Speed: 526 knots, 604.9 mph, 974.152 km/h
Operational Ceiling: 22,950 ft. / 6,995 M

Armament

1 x 30mm cannon, bombs, laser guided bombs, rockets, ASMs, or gun pods

 

 

 


 

 

 

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 pilotís 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 pilotís cockpit

         The aircraft is equipped with higher-duty engines with less IR radiation.

 

 

 

Specification and photos are not contractual and are subject to verification upon inspection

 

NB: Aircraft offered for sale subject to contract, prior sale, withdrawal from the market and information regarding any aircraft or helicopter and provided verbally or in written documentation and/or contained within this email or associated paper-work should be taken as a guide only in determining the suitability, including that aircraft or helicopters specification and/or performance.  We highly recommend that any buyer or lessee perform their own inspections and due diligence to verify any and all technical, performance and specification information contained therein including OEM claims.

 

PLEASE NOTE: AIRCRAFT SPECIFICATIONS SUBJECT TO VERIFICATION UPON INSPECTION. WE DO NOT ACCEPT ANY LIABILITY FOR AIRCRAFT DEFECTS, HISTORY OR TECHNICAL RECORD ERRORS. IT IS THE BUYERS RESPONSIBILITY TO INDEPENDENTLY VERIFY THE AIRCRAFT AND COMPONENT HISTORY.

 

 

 

TAKE NOTICE!

 

PLEASE BE ADVISED THAT INFORMATION INCLUDED IS CONFIDENTIAL IN NATURE AND IS BASED ON PRE-EXISTING BUSINESS RELATIONSHIP WITH THE LEGAL OWNER OF PROPERTY DESCRIBED HEREIN (IF APPLICABLE). AS SUCH, UPON RECEIPT OF SAID INFORMATION THE RECEIVER ACKNOWLEDGES THAT ANY UNAUTHORIZED CONTACT WITH SAID LEGAL SELLER WILL BE CHARACTERIZED AS A BREACH OF CONFIDENTIALITY AND SAID AGREEMENT MAY BE ENFORCED UNDER EXISTING LAW OR IN EQUITY.

 

This paper was prepared by General Equipment Inc.
The paper represents an offer of a partner of General Equipment Inc.
All rights are reserved by and for General Equipment Inc.
All content and ideas of this paper are the property of General Equipment Inc.

 

 

 


 

 

Defense items are subject to final destination approval and granting of an

export license issued by exporting country's authorities