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Sukhoi Su - 25 ( frogfoot ) - fighter for close air support
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Sukhoi Su-25 (frogfoot) - fighter for close air support

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INTRODUCTION

• The Sukhoi Su-25 (NATO reporting name: "Frogfoot") is a single-seat, twin-engine

jet aircraft developed in the Soviet Union by the Sukhoi Design Bureau.

• It was designed to provide close air support for the Soviet Ground Forces.

• The first prototype made its maiden flight on 22 February 1975. After testing, the

aircraft went into series production in 1978 at Tbilisi in the Soviet Republic of

Georgia.

• Russian air and ground forces nicknamed it "Gratch" ("Rook").

• Early variants included the Su-25UB two-seat trainer, the Su-25BM for target-

towing, and the Su-25K for export customers. Some aircraft are being upgraded to

version Su-25SM as of 2012.

• The Su-25T and the Su-25TM (also known as Su-39) were further developments, not

produced in numbers. The Su-25, and the Su-34, were the only armoured fixed-

wing aircraft in production in 2007.

• Su-25 is in service with Russia, other CIS states, and export customers.

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COCKPIT

• The pilot flies the aircraft by means of a centre stick and left hand throttles.

• The pilot sits on a Zvezda K-36 ejection seat (similar to the Sukhoi Su-27),and has standard flight instruments. At the rear of the cockpit is a 6 mm (0.24in) thick steel headrest, mounted on the rear bulkhead.

• The cockpit has a bathtub-shaped armoured enclosure of welded titaniumsheets, with transit ports located in the walls. Guide rails for the ejection seatare mounted on the rear wall of the cockpit.

• The canopy hinges open to the right, and the pilot enters using the flip-downladder. Once inside, the pilot sits low in the cockpit, protected by the bathtubassembly, which makes for a cramped cockpit.

• Visibility from the cockpit is limited, being a trade-off for improved pilotprotection. Rearwards visibility is very limited, though a periscope is fitted ontop of the canopy to compensate.

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AVIONICS

• The base model Su-25 incorporates a number of key avionics systems. It hasno TV guidance, but includes a distinctive nose-mounted laser rangefinder,that is hypothesized to provide for laser-based target designation capability.

• A DISS-7 doppler radar is used for navigational purposes; the Su-25 can fly atnight, in both visual and instrument meteorological conditions.

• The Su-25 often has multiple radios installed for air-to-ground and air-to-aircommunications, including an SO-69 identification-friend-or-foe (IFF)transponder.

• The aircraft's self-defence suite includes various measures, such as flare andchaff dispensers capable of launching up to 250 flares and dipole chaff. Hostileradar uses are guarded against via an SPO-15 radar warning receiver.

• An airtight avionics compartment is behind the cockpit and in front of theforward fuel tank.

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DESIGN

• The Su-25 has a conventional aerodynamic layout with a shoulder-mounted

trapezoidal wing and a traditional tailplane and rudder.

• Several different metals are used in the construction of the airframe: 60% aluminium,

19% steel, 13.5% titanium, 2% magnesium alloy, and 5.5% other materials.

• All versions of the Su-25 have a metal cantilever wing, of moderate sweep and high

aspect ratio, and equipped with high-lift devices.

• The wing consists of two cantilever sections attached to a central torsion box,

forming a single unit with the fuselage.

• The air brakes are housed in separate fairings at the tip of each wing. Each wing has

five hardpoints for weapons carriage, with the attachment points mounted on load-

bearing ribs and spars.

• Each wing also features a five-section leading edge slat, a two-section flap, and an

aileron.

• The flaps are mounted by steel sliders and rollers, attached to brackets on the rear

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SPECIFICATIONS

• Crew: one

• Length: 15.53 m[nb 1] (50 ft 111⁄2 in)

• Wingspan: 14.36 m (47 ft 11⁄2 in)

• Height: 4.80 m (15 ft 9 in)

• Wing area: 33.7 m² (323 ft²)

• Empty weight: 9,800 kg (21,605 lb)

• Loaded weight: 14,600 kg (32,187 lb) (normal take-off weight)

• Max. takeoff weight: 17,600 kg (38,800 lb)

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REFERENCES

• http://risewall.com/sukhoi-su-25-images.html

• http://gamingshogun.com/wp-content/uploads/2013/07/Su-25-1.png

• http://www.fantom-xp.com/wp_14_~_Su-25_Frogfoot-A.html

• http://www.rusarmy.com/photo/avia0/samoleti/su-25/su-25t%20002.jpg

• http://wall4all.me/wallpaper/759810-25-Frogfoot-aircraft-military

• http://cdn-www.airliners.net/aviation-photos/photos/0/3/9/1688930.jpg

• http://img2.wikia.nocookie.net/__cb20120404021541/acecombat/images/4/46/ACAH_Su-25_Profil.jpg

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THANK YOU