| Aeroprogress | |
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HW100 - 45000
UAW55 - 105000 RRW100 - 175000 PKRR - 7500 |
Aeroprogress Aeroprogress Industry - Aerospace Founded - 1990 Headquarters - Moscow, Russia Products - Military, transport and civilian aircraft Aeroprogress is a Russian aircraft design company based in Moscow. Aircraft are certified by subsidiary company the ROKS-AERO Aviation Design Bureau. Aircraft T-101 Gratch A passenger and cargo aircraft first flown in 1994 and manufactured by MAPO-MiG, powered by a TVD-10B turboprop. T-201 Aist First flown in 1995 a single-engine STOL utility aircraft powered y a Pratt & Whitney Canada PT6-67K turboporop. T-203 Pchel An agricultural variant of T-201 with low-mounted wings and spray-bars. T-411 Aist Light utility monoplane manufactured by the Khrunichev State Research and Production Space Center. Marketed in the US as the "Aeroprogress T-411 Wolverine". Projects T-106 Twin-engined variant of the T-101. T-110 Lengthened variant of the T-106. T-112 Cargo variant of the T-106 with a rear ramp. T-121 Grif Single-engined high-wing utility aircraft powered by a TVD=10B turboprop. T-130 Fregat Amphibious flying-boat with room for 15 passengers. T-132 Amphibious flying-boat variant of the T106. T-134 Variant of the T-130 for coast guard use. T-204 Progress Twin-engined passenger/cargo aircraft for 9-12 passengers. T-205 PT6A powered utility aircraft. T-401 Sokol Light general-purpose high-wing aircraft. T-407 Skborets Single-engined Light utility aircraft, prototype built by Krunichev. T-433 Flamingo Five-seat light amphibious flying boat. T-435 Korvet Variant of the T-433 with conventional landing gear. T-501 Strizh 1990s project for a two-seat basic trainer for the Russian Air Force, to be powered by a single OMSK/Glushenkov TVD-10B turboprop. With a length of 9.66 metres (31 ft 8 in) and span of 11.0 metres (36 ft 1 in), estimated takeoff weight was 2,670 kilograms (5,890 lb), maximum speed 570 kilometres per hour (350 mph) and range 1,800 kilometres (1,100 mi). In 1992 three prototypes were under construction by MAPO-MIG, while it was intended that production aircraft would have been built by Khrunichev. T-504 Borets A Twin-seat twin-boom design for a combat trainer powered by two TVD-10B turoprops. T-610 Voyage STOL multi-purpose single-engined utility aircraft. T-710 Anaconda Two-seat all-weather STOL strike aircraft. T-720 Lightweight two-seat combat aircraft powered by a TVD-1500 turboprop driving a six-bladed pusher propeller. T-730 Two-seat light attack aircraft and trainer powered by a Soyuz TVD-450 turoprop driving a 6-bladed pusher propeller. T-752 Shytk Wing-in-ground-effect strike aircraft powered by two Klimov TV7-117M2 turboprops. T-910 Kuryer Single turbofan powered business jet. ROS-Aeroprogress T-101 Grach T-101 Grach Role - Light utility monoplane National origin - Russia Manufacturer - Krunichev OKB Designer - Evgeny Grunin First flight - December 7, 1994 Number built - 2 The light multipurpose aircraft T-101 "Grach" or "Rook" in English, was based on the An-2 biplane and planned as a replacement for it. The design is focused on low cost, high reliability, and operating from unprepared airfields. The T-101 can carry 10 passengers, or transport 1600 kg of cargo. It can be used for agricultural, patrol, aerial photography, search and rescue, airborne and other utility functions. The T-101 has a strut-braced high-wing, fixed landing gear with tail wheel and a single engine in the nose. Specifications Data from Jane's all the World's Aircraft 2004-05 General characteristics Crew: 1 or 2 Length: 15.06 m (49 ft 5 in) Wingspan: 18.2 m (59 ft 9 in) Height: 4.86 m (15 ft 11 in) Wing area: 43.63 m2 (469.6 sq ft) Aspect ratio: 7.6 Airfoil: TsAGI P-11-14; 3° dihedral ; 3° incidence Empty weight: 3,330 kg (7,341 lb) Max takeoff weight: 5,250 kg (11,574 lb) Fuel capacity: 1,200 l (320 US gal; 260 imp gal) / 950 kg (2,090 lb) max Powerplant: 1 × Glushenkov TVD-10B (Omsk / Mars TVD-10) turboprop, 706 kW (947 shp) Propellers: 3-bladed AV-24N, 2.8 m (9 ft 2 in) diameter constant-speed fully-feathering reversible propeller Performance Maximum speed: 300 km/h (190 mph, 160 kn) at 3,000 m (9,800 ft) Cruise speed: 250 km/h (160 mph, 130 kn) at 3,000 m (9,800 ft) Range: 700 km (430 mi, 380 nmi) with max payload: 1,270 km (790 mi; 690 nmi) with max fuel Service ceiling: 4,000 m (13,000 ft) Wing loading: 120.3 kg/m2 (24.6 lb/sq ft) Power/mass: 7.44 kg/kW (12.22 lb/shp) |