| Název: Name: | Mikojan-Gurevič MiG-29SMT (9-17) | Mikoyan-Gurevich MiG-29SMT (9-17) |
| Originální název: Original Name: | Микоян-Гуревич МиГ-29СМТ (9-17) | |
| Kategorie: Category: | víceúčelový bojový letoun | multi-role combat aeroplane |
| Výrobce: Producer: | DD.MM.1999-DD.MM.1999 Moskevské letecké výrobní sdružení MiG, Moskva | |
| Období výroby: Production Period: | DD.MM.1999-DD.MM.1999 (sériová výroba nezahájena / serial production not started) | |
| Vyrobeno kusů: Number of Produced: | 1 prototyp / prototype | |
| První vzlet: Maiden Flight: | DD.01.1999 MiG-29SMT ("917") | |
| 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: | 11600 kg | 25574 lb |
| Vzletová hmotnost: Take-off Weight: | 16850 kg | 37148 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 21000 kg | 46297 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: | 4835 kg | 10659 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: | 18000 m | 59055 ft |
| Dolet: Range: | 22001) km | 13671) mi |
| Maximální dolet: Maximum Range: | 34002) km | 21132) mi |
| Výzbroj: Armament: | kanón GŠ-301 se zásobou 150 nábojů maximální hmotnost výzbroje 4000 kg na 6 (7) závěsnících 2x R-27ER / R-27ET 2x R-27R1 / R-27T1 6x R-77 6x R-60M 6x R-73 4x Ch-25ML 2x Ch-29L 2x Ch-29T 2x Ch-31A 2x Ch-31P 4x B-8M1 4x S-24 4x KAB-500Kr 8x FAB-250 4x FAB-500 4x KMGU 1x PTB-1500 2x PTB-1150 | GSh-301 gun with 150 rounds of ammunition maximum armament weight of 8818 lb on 6 (7) hardpoints 2x R-27ER / R-27ET 2x R-27R1 / R-27T1 6x R-77 6x R-60M 6x R-73 4x Kh-25ML 2x Kh-29L 2x Kh-29T 2x Kh-31A 2x Kh-31P 4x B-8M1 4x S-24 4x KAB-500Kr 8x FAB-250 4x FAB-500 4x KMGU 1x PTB-1500 2x PTB-1150 |
| Uživatelské státy: User States: | - | - |
| Poznámka: Note: | 1) ve velké výšce 2) se třemi přídavnými nádržemi, 6700 km se třemi přídavnými nádržemi a jedním doplňováním paliva za letu kódové označení NATO: Fulcrum-F | 1) at high altitude 2) with three external fuel tanks, 4163 mi with three external fuel tanks and one in-flight refuelling NATO reporting name: Fulcrum-F |
| 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/mig29smt.html ruslet.webnode.cz | |
Mikojan-Gurevič MiG-29SMT (9-17) [kód NATO: Fulcrum-F]
Mikoyan-Gurevich MiG-29SMT (9-17)
Микоян-Гуревич МиГ-29СМТ (9-17)
MiG-29SMT (sections 9-17)
Single-seat tactical multi-purpose fighter, further improved version of the variant MiG-29SM (9-13SM). Compared to the previous version, the avionics was improved, the range of usable weapons was further expanded and the range was increased. The first version of the MiG-29SMT designed for the Russian Air Force had an improved radar N019MP with a surface mapping mode, further improved communication capabilities, a system of electronic countermeasures and a system for recording flight data. In addition, the cockpit was modified, including the addition of two color LCD displays with button control, the controls were arranged to conform to the principle of HOTAS (Hands on Throttle and Stick). Another advantage was the extended service life. The range of usable weapons has grown by missiles Ch-31A, Ch-31P and Ch-29T and guided bombs KAB-500Kr. The fuel supply increased by more than 40 percent, in addition, the aircraft was equipped with a removable attachment for in-flight refueling.
At the end of the 1990s, a total of three prototypes were prepared. The first was designed for tests of the new cockpit layout (No. 405, first takeoff on November 9, 1997), the other for testing radar N019MP (No. 404, September 1997), the last for testing the new fuel system and for testing a completely modernized MiG-29SMT 9-17), this machine had the number 917 (possibly number 47-10) and was ready on July 14, 1998. This was followed by the conversion of the first, but also the last machine of the Russian Air Force to the MiG-29SMT standard, which ended in 1999. however, conversions of other machines did not continue.
Source:
Single-seat tactical multi-purpose fighter, further improved version of the variant MiG-29SM (9-13SM). Compared to the previous version, the avionics was improved, the range of usable weapons was further expanded and the range was increased. The first version of the MiG-29SMT designed for the Russian Air Force had an improved radar N019MP with a surface mapping mode, further improved communication capabilities, a system of electronic countermeasures and a system for recording flight data. In addition, the cockpit was modified, including the addition of two color LCD displays with button control, the controls were arranged to conform to the principle of HOTAS (Hands on Throttle and Stick). Another advantage was the extended service life. The range of usable weapons has grown by missiles Ch-31A, Ch-31P and Ch-29T and guided bombs KAB-500Kr. The fuel supply increased by more than 40 percent, in addition, the aircraft was equipped with a removable attachment for in-flight refueling.
At the end of the 1990s, a total of three prototypes were prepared. The first was designed for tests of the new cockpit layout (No. 405, first takeoff on November 9, 1997), the other for testing radar N019MP (No. 404, September 1997), the last for testing the new fuel system and for testing a completely modernized MiG-29SMT 9-17), this machine had the number 917 (possibly number 47-10) and was ready on July 14, 1998. This was followed by the conversion of the first, but also the last machine of the Russian Air Force to the MiG-29SMT standard, which ended in 1999. however, conversions of other machines did not continue.
Source:
AFM January 2007, Annex MiG-29, Andrey Fomin
Reklama
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http://aviadejavu.ru/Site/Crafts/Craft20586.htm
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| Type | Mikojan-Gurevič MiG-29SMT (9-17) [kód NATO: Fulcrum-F] |
| Camouflage | - |
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| Date (DD.MM.RRRR) | DD.MM.RRRR |
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