MIG-21 (NOT FLYWORTHY)

We sell the high flying Soviet military aircraft MiG-21 for exhibition purposes (not flyworthy). Buy a number (twenty) one Red Army fighter jet MiG-21. We're also selling Mil Mi-2 helicopters. MiG-21 drawing with dimensions MiG-21 in Czechoslovakia The MiG-21 fighter entered the Czechoslovak Air Force on the basis of the plan of air force development until 1960. In the late 50s of the 20th century, this type was selected as a counterweight to the F-104 Starfighter, which the German Luftwaffe in the early 60s of the 20th century. planned to put into service. After a bilateral agreement with the Soviet Union, serial production of the MiG-21F-13 version began at the Aero Vodochody factory. As part of the agreement, 4 MiG-21F-13s were disassembled from the USSR in disassembled condition and one sample unit as a whole. These machines were to be used to gain the necessary experience associated with production processes and maintenance. The first Czechoslovak serial piece had the serial number 360101 and was manufactured in 1963. The aircraft was assigned to the airport Mladá u Milovic in the autumn of 1963. Production was terminated in Vodochody on June 17, 1972, when the last machine with serial number 261114 was flown. production company produced 195 aircraft. Parameter: MiG-21F (product 72) / MiG-21F13 (product 74) MiG-21M (Product 96) MiG-21MF (Product 96F) MiG-21SPS / SPS-K (product 94 / 94K) crew 1 length 15.76 m 13.85 m span 7.15 m height 4.10 m 4.12 m 4.13 m Wing area 22.95 m² 23.00 m² 22.95 m² Wing extension 2.23 2.22 2.23 Wing loading minimal: 217 kg / m² maximum: 376 kg / m² minimal: 259 kg / m² maximum: 409 kg / m² minimal: 261 kg / m² nominal: 357 kg / m² maximum: 409 kg / m² maximum: 339 kg / m² Empty mass 4870 kg 5950 kg 6000 kg 5411 kg normal starting mass 7110 kg 8950 kg 8200 kg 7575 kg Max. Starting mass 8625 kg 9400 kg 9080 kg Fuel supply internal: 2470 l external: 490 l   normal: 2650 l maximum 4070 l normal: 2750 l Top speed 2125 km / h (at an altitude of 12,500 m) 2230 km / h (at an altitude of 11,000 m) 1100 km / h (at sea level) 2230 km / h (at an altitude of 11,000 m) 1300 km / h (at sea level) 2175 km / h March speed 1100 km / h   1200 km / h 1250 km / h Landing speed 260-270 km / h 270 km / h 230 km / h Rate of climb 130 m / s k. A. 180 m / s 210 m / s Service summit height 17,500 m 18,500 m 19,000 m 19,900 m Range normal: 1300 km maximum: 1640 km normal: 1100 km maximum: 1800 km normal: 1370 km maximum: 1800 km Take-off runway 800 m     850-1350 m Landing taxiway with umbrella: 550 m without umbrella: 1100 m   550 m 420-500 m Engine (here for NVA) a Turbojet Tumanski R-11 F-300 a Turbojet Tumanski R-11-F2SK-300 or after conversion 1 × R-13-300 a Turbojet Tumanski R- 13-300 a Turbojet Tumanski R-11-F2S-300 Thrust with afterburner: 57.48 kN without afterburner: 38.25 kN with afterburner: 60.60 kN without afterburner: 38.30 kN with afterburner: 60.70 kN without afterburner: 40.30 kN with afterburner: 56.40 kN without afterburner: 42.25 kN Thrust-to-weight ratio maximum: 1.18 minimal: 0.68 maximum: 1.04 minimal: 0.66 maximum: 1.03 nominal: 0.75 minimal: 0.66   minimal: 0.74