| Název: Name: | Mikojan-Gurevič MiG-29 (9-12) | Mikoyan-Gurevich MiG-29 (9-12) |
| Originální název: Original Name: | Микоян-Гуревич МиГ-29 (9-12) | |
| Kategorie: Category: | stíhací letoun | fighter aeroplane |
| Výrobce: Producer: | DD.MM.1982-DD.MM.1986 Moskevské letecké výrobní sdružení, Moskva | |
| Období výroby: Production Period: | DD.MM.1982-DD.MM.1986 (série 9-12 pro SSSR / 9-12 series for the USSR) | |
| Vyrobeno kusů: Number of Produced: | 779 (všechny letouny řady 9-12, 9-12A, 9-12B) / 779 (all aicraft of 9-12, 9-12A, 9-12B series) | |
| První vzlet: Maiden Flight: | 06.10.1977 (prototyp "901" / prototype "901") | |
| Osádka: Crew: | 1 | |
| Základní charakteristika: Basic Characteristics: | ||
| Vzlet a přistání: Take-off and Landing: | CTOL - konvenční vzlet a přistání | CTOL - conventional take-off and landing |
| Uspořádání křídla: Arrangement of Wing: | jednoplošník | monoplane |
| Uspořádání letounu: Aircraft Concept: | klasické | conventional |
| Podvozek: Undercarriage: | zatahovací | retractable |
| Přistávací zařízení: Landing Gear: | kola | wheels |
| Technické údaje: Technical Data: | ||
| Hmotnost prázdného letounu: Empty Weight: | 10900 kg | 24030 lb |
| Vzletová hmotnost: Take-off Weight: | 15000 kg | 33069 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 18480 kg | 40741 lb |
| Rozpětí: Wingspan: | 11,36 m | 37ft 3in |
| Délka: Length: | 17,32 m | 56ft 10in |
| Výška: Height: | 4,73 m | 15ft 6in |
| Plocha křídla: Wing Area: | 38,056 m2 | 409.63 ft2 |
| Plošné zatížení: Wing Loading: | ? kg/m2 | ? lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | dvouproudový | turbofan |
| Počet motorů: Number of Engines: | 2 | |
| Typ: Type: | Klimov RD-33 - maximální tah bez přídavného spalování: 49,43 kN - maximální tah s přídavným spalováním: 81,79 kN | Klimov RD-33 - maximum thrust, dry: 11111 lbf - maximum thrust, afterburning: 18387 lbf |
| Objem palivových nádrží: Fuel Tank Capacity: | 3630 kg | 8003 lb |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 2450 km/h v 11000 m | 1522 mph in 36089 ft |
| Cestovní rychlost: Cruise Speed: | ? km/h v ? m | ? mph in ? ft |
| Rychlost stoupání: Climb Rate: | 330 m/s | 64961 ft/min |
| Čas výstupu na výšku: Time to Climb to: | ? min do ? m | ? min to ? ft |
| Operační dostup: Service Ceiling: | 17500 m | 57415 ft |
| Dolet: Range: | 15001) km | 9321) mi |
| Maximální dolet: Maximum Range: | 29002) km | 18022) mi |
| Výzbroj: Armament: | kanón GŠ-301 se zásobou 150 nábojů maximální hmotnost výzbroje 3200 kg na 6 (7) závěsnících 2x R-27R 6x R-60M 6x R-73 4x B-8M1 4x S-24 6x FAB-250 6x FAB-500 4x KMGU 4x ZB-500 1x PTB-1500 2x PTB-1150 | GSh-301 gun with 150 rounds of ammunition maximum armament weight of 7055 lb on 6 (7) hardpoints 2x R-27R 6x R-60M 6x R-73 4x B-8M1 4x S-24 6x FAB-250 6x FAB-500 4x KMGU 4x ZB-500 1x PTB-1500 2x PTB-1150 |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | 1) palivo ve vnitřních nádržích 2) se třemi přídavnými nádržemi kódové označení NATO: Fulcrum-A | 1) on internal fuel 2) with three external fuel tanks NATO reporting name: Fulcrum-A |
| Zdroje: Sources: | Jakubovič, N.: MiG-29 - Istrebitěl "nevidimok", Jauza, EKSMO, 2010 Gordon, Y.: Mikoyan MiG-29: Famous Russian Aircraft, Ian Allan Publishing, 2010 http://www.airwar.ru/enc/fighter/mig29.html ruslet.webnode.cz | |
Mikojan-Gurevič MiG-29 (9-12) [kód NATO: Fulcrum-A]
Mikoyan-Gurevich MiG-29 (9-12)
Микоян-Гуревич МиГ-29 (9-12)
MiG-29 (divisions 9-12)
The basic model of the MiG-29 entered service in the Soviet Air Force in 1984. The first aircraft number 901 (9-12/1) took off on October 6, 1977. Between 1977 and 1982, a total of 14 test and development pieces were built. The aircraft were manufactured in the factory of the MiG design office in Moscow and in the MAPO production plant. Both factories are now in RAC MiG Corp. Official state exams began in 1979 and ended in October 1983, with a total of 2330 flights. The official date of entry into service was set for June 11, 1987. This variant served in the Air Force of the Soviet Union, is now in service with Russia, Belarus, Ukraine, Kazakhstan, Turkmenistan, Uzbekistan.
Version 9-12 differs from the following models by a smaller leading edge of the vertical tail surfaces. In 1995, one original 9-12 machine was used as a MiG-29SD for in-flight refueling tests. Later, Malaysia's 16 single-seater aircraft were equipped with this system.
Source:
The basic model of the MiG-29 entered service in the Soviet Air Force in 1984. The first aircraft number 901 (9-12/1) took off on October 6, 1977. Between 1977 and 1982, a total of 14 test and development pieces were built. The aircraft were manufactured in the factory of the MiG design office in Moscow and in the MAPO production plant. Both factories are now in RAC MiG Corp. Official state exams began in 1979 and ended in October 1983, with a total of 2330 flights. The official date of entry into service was set for June 11, 1987. This variant served in the Air Force of the Soviet Union, is now in service with Russia, Belarus, Ukraine, Kazakhstan, Turkmenistan, Uzbekistan.
Version 9-12 differs from the following models by a smaller leading edge of the vertical tail surfaces. In 1995, one original 9-12 machine was used as a MiG-29SD for in-flight refueling tests. Later, Malaysia's 16 single-seater aircraft were equipped with this system.
Source:
AFM January 2007, Annex MiG-29, Andrey Fomin
Reklama
http://www.airwar.ru/enc/fighter/mig29.html
.![Mikojan-Gurevič MiG-29 (9-12) [kód NATO: Fulcrum-A] -](/attachments/217/mig29-1.jpg)
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