| Název: Name: | Mikojan-Gurevič MiG-25RU | Mikoyan-Gurevich MiG-25RU |
| Originální název: Original Name: | Микоян и Гуревич МиГ-25РУ | |
| Kategorie: Category: | cvičný letoun | trainer aeroplane |
| Výrobce: Producer: | DD.MM.1972-DD.MM.1982 Gorkovský letecký závod Ordžonikidzeho, Gorkij | |
| Období výroby: Production Period: | DD.MM.1972-DD.MM.1982 | |
| Vyrobeno kusů: Number of Produced: | 48 | |
| První vzlet: Maiden Flight: | 20.03.1970 | |
| Osádka: Crew: | 2 | |
| 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: | 18760 kg | 41359 lb |
| Vzletová hmotnost: Take-off Weight: | 32100 kg | 78639 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 39200 kg | 86421 lb |
| Rozpětí: Wingspan: | 13,42 m | 44ft 0,35in |
| Délka: Length: | 21,55 m | 70ft 8,42in |
| Výška: Height: | 6,50 m | 21ft 3,9in |
| Plocha křídla: Wing Area: | 61,40 m2 | 660.9 ft2 |
| Plošné zatížení: Wing Loading: | 512,121 kg/m2 | 104.89 lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | jednoproudový | turbojet |
| Počet motorů: Number of Engines: | 2 | |
| Typ: Type: | R-15B-300 (Р-15Б-300) - maximální tah bez přídavného spalování: 73,5 kN - maximální tah s přídavným spalováním: 109,8 kN | R-15B-300 (Р-15Б-300) - maximum thrust, dry: 16523 lbf - maximum thrust, afterburning: 24684 lbf |
| Objem palivových nádrží: Fuel Tank Capacity: | ? | ? |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 3000 km/h v 13000 m | 1864 mph in 42651 ft |
| Cestovní rychlost: Cruise Speed: | ? km/h v ? m | ? mph in ? ft |
| Rychlost stoupání: Climb Rate: | ? m/s | ? ft/min |
| Čas výstupu na výšku: Time to Climb to: | ? min do ? m | ? min to ? ft |
| Operační dostup: Service Ceiling: | 20000 m | 65617 ft |
| Dolet: Range: | ? km | ? mi |
| Maximální dolet: Maximum Range: | 2400 1) km | 1491 1) mi |
| Výzbroj: Armament: | - | - |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | kódové označení NATO: Foxbat-C 1) maximální přeletová vzdálenost | NATO reporting name: Foxbat-C 1) ferry range |
| Zdroje: Sources: | Gordon, Y., Komissarov, D.: Mikoyan MiG-25 Foxbat: Guardian of Soviet Borders, Ian Allan, 2007 http://www.airwar.ru/enc/other/mig25ru.html | |
Mikojan-Gurevič MiG-25RU [kód NATO: Foxbat-C]
Mikoyan-Gurevich MiG-25RU
Микоян-Гуревич МиГ-25РУ
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Mikoyan MiG-25RU Side view by Basil Zolotov
![Mikojan-Gurevič MiG-25RU [kód NATO: Foxbat-C] - Source : http://basilzolotov.com](/attachments/121/mig-25u-36-x_1_.png)
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Source : http://basilzolotov.com
Reklama
This post has not been translated to English yet. Please use the TRANSLATE button above to see machine translation of this post.
Mikoyan MiG-25RU Side view by Basil Zolotov
![Mikojan-Gurevič MiG-25RU [kód NATO: Foxbat-C] - Source : http://basilzolotov.com](/attachments/121/mig-25u-33-x1_1_.png)
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Source : http://basilzolotov.com
This post has not been translated to English yet. Please use the TRANSLATE button above to see machine translation of this post.
![Mikojan-Gurevič MiG-25RU [kód NATO: Foxbat-C] - (autor neznámý, via Internet)](/attachments/121/MiG-25RU_Indie.jpeg)
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(autor neznámý, via Internet)
Test katapultovacej seats.
source:
.
![Mikojan-Gurevič MiG-25RU [kód NATO: Foxbat-C] -](https://vcdns.valka.cz/attachments/12801/thumbs/ezppZmG.jpg)
source:
www.reddit.com
. ![Mikojan-Gurevič MiG-25RU [kód NATO: Foxbat-C] -](/attachments/12801/ezppZmG.jpg)
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| Type | Mikojan-Gurevič MiG-25 [kód NATO: Foxbat] |
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Reklama
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