(1974-present) (tactical bomber/interdictor)
Belarus - Air Force
A Russian Su-24 Fencer making a low pass.
Hi all This is what I'm doing a conversion from a Su-27UB Flanker C Minihobby 1:48th for a Sukhoi Su-34 Fullback. I took some pictures as a reference and a plant sized to scale.
It was an investment in a lot more time & moolah than I ever expected. All you guys, my LSP friends made the journey worth it. It took me way longer than expected (as always ) but I like the results. This is my version of the Russian test bed Sukhoi SU-30 MKK Flanker as it existed prior to de...
Személyes makettező blog / Personal scale modeling blog
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Follow me at facebook.com/hermercraftTaken from pmodel.net/en
a 2X4, 16 inches block of wood carved, to a Sukhoi 27 Russian fighter aircraft to its details. body is made of pine wood, wings and flaps made of poplar, sta...
Photo taken at Primorsko - Akhtarsk (URKP) in Russia on August 23, 2010.
Sukhoi PAK-FA abbreviated in Russian language as Prospective Airborne Complex of Front line Aviation is a program to develop fifth generation fighter aircraft. The prototype aircraft designated as T...
Explore MichaelHind's 3568 photos on Flickr!
Description Sukhoi SU-51 UB General characteristics * Crew: 1 * Length: 19.8 m (65.9 ft) * Wingspan: 14 m (46.6 ft) * Height: 6.05 m (19.8 ft) * Wing area: 78.8 m2 (848.1 ft2) * Empty weight: 18,500 kg (40,785 lb) * Loaded weight: 26,000 kg (57,320 lb) * Useful load: 7,500 kg (combat load) (16,534 lb) * Max takeoff weight: 37,000 kg (81,570 lb) * Powerplant: 2× New unnamed engine by NPO Saturn and FNPTS MMPP Salyut of 175 kN each. Prototype with AL-41F1 of 147 kN each,[65] definitive version with new engine >157 kN[65] * Fuel capability: 10,300 kg (22,711 lb)[63] * Minimum Radar Cross Section (RCS): 0.5 m²[66] Performance * Maximum speed: 2,100 - 2,500 km/h (Mach 2+) [63][67] (1,300 - 1,560 mph) ; at 17,000 m (45,000 ft) altitude * Cruise speed: 1,850 - 2,100 km/h [67] (1,150 - 1,300 mph) * Ferry range: 5,500 km[68] (3417 miles) * Service ceiling: 20,000 m (65,616 ft) * Rate of climb: 350 m/sec (68,900 ft/min) * Wing loading: 330(normal) - 470(maximum) kg/m2 (67(normal) - 96(maximum) lb/ft2) * Thrust/weight: 1.19 [63] * Maximum g-load: 10-11 g[63] Armament * Guns: None on prototype. Apparent provision for a cannon (most likely GSh-301).Possible two 30mm cannons[26] * Hardpoints: Two internal bays estimated at 4.6-4.7 metres by 1-1.1 metres.[69] Other sources suggest two auxiliary internal bays for short range AAMS and six external hardpoints Avionics N050(?)BRLS AFAR/AESA built by Tikhomirov NIIP and based on Tikhomirov NIIP N035 Irbis-E. It will be the second aircraft based AESA Radar to be built by Russia, the first being the Phazotron NIIR ZHUK-A Radar in the MIG-35.[70] [edit] Designed armament Two Izdeliye 810 Extended beyond visual range missiles per weapons bay. Multiple Izdeliye 180 / K77M beyond visual range missiles. K74 and K30 within visual range missiles can also be carried.[69] Two KH38M or KH58 USHK air-to-ground missiles per weapons bay. Multiple 250–500 kg precision guided bombs per weapons bay,[69] with a maximum of 10 bombs in internal bays[71] Other possible loads include one 1500 kg bomb per weapons bay or two 400 km+ range anti-AWACS weapons on external hard-points.[68] A maximum weapons load of 7500 kg is reported.[71]
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