Název: Name: | Suchoj Su-3 | |
Originální název: Original Name: | Сухой Су-3 | |
Kategorie: Category: | stíhací letoun | |
Výrobce: Producer: | DD.MM.1941-DD.04.1941 Novosibirský letecký závod č. 153 V. P. Čkalova, Novosibirsk / | |
Období výroby: Production Period: | 17.01.1941-DD.04.1941 | |
Vyrobeno kusů: Number of Produced: | 1 | |
První vzlet: Maiden Flight: | DD.05.1941 | |
Osádka: Crew: | 1 | |
Základní charakteristika: Basic Characteristics: | ||
Vzlet a přistání: Take-off and Landing: | CTOL - konvenční vzlet a přistání | |
Uspořádání křídla: Arrangement of Wing: | jednoplošník | |
Uspořádání letounu: Aircraft Concept: | klasické | |
Podvozek: Undercarriage: | zatahovací | |
Přistávací zařízení: Landing Gear: | kola | |
Technické údaje: Technical Data: | ||
Hmotnost prázdného letounu: Empty Weight: | 2496 kg | |
Vzletová hmotnost: Take-off Weight: | 2992 kg | |
Maximální vzletová hmotnost: Maximum Take-off Weight: | ? kg | |
Rozpětí: Wingspan: | 10,100 m | |
Délka: Length: | 8,420 m | |
Výška: Height: | 2,710 m | |
Plocha křídla: Wing Area: | 18,00 m2 | |
Plošné zatížení: Wing Loading: | 166,22 kg/m2 | |
Pohon: Propulsion: | ||
Kategorie: Category: | pístový | |
Počet motorů: Number of Engines: | 1 | |
Typ: Type: | Klimov M-105P kapalinou chlazený vidlicový dvanáctiválec, přeplňovaný dvěma turbokompresory TK-2, vzletový výkon 809 kW ( 1 100 k). Vrtule trojlistá stavitelná VIŠ-61. | |
Objem palivových nádrží: Fuel Tank Capacity: | 340 l + 200 l v přídavné nádrži pod levým křídlem | |
Výkony: Performance: | ||
Maximální rychlost: Maximum Speed: | 638 km/h v 10000 m | |
Cestovní rychlost: Cruise Speed: | 570 km/h v ? m | |
Rychlost stoupání: Climb Rate: | 15,7 m/s | |
Čas výstupu na výšku: Time to Climb to: | 5,1 min do 5000 m | |
Operační dostup: Service Ceiling: | 11900 m | |
Dolet: Range: | 700 km | |
Maximální dolet: Maximum Range: | ? km | |
Výzbroj: Armament: | 1x pevný kanón ŠVAK ráže 20 mm střílející osou vrtule se 190 náboji a 2x pevný synchronizovaný kulomet ŠKAS ráže 7,62 mm nad motorem po 900 nábojích. | |
Uživatelské státy: User States: | - | |
Poznámka: Note: | Prototyp výškového stíhače. | |
Zdroje: Sources: | Vladimir Antonov, Yefim Gordon and others, OKB Sukhoi, Leicester, Midland, 1996, ISBN 1-85780-012-5 Václav Němeček, Vojenská letadla 3 díl, druhé doplněné vydání, Naše Vojsko, Praha 1992, ISBN 80-206-0117-1 www.aviarmor.net http://www.sukhoi.org/eng/planes/museum/su1_3/ school415.narod.ru http://www.sukhoi.org/planes/museum/su1_3/ http://www.airwar.ru/enc/fww2/su3.html |
URL : https://www.valka.cz/Suchoj-Su-3-t724#116376Version : 0
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History:
In 1941, the kharkov aviation plant had to move to the city of Novosibirsk, the prototype Su-1 was destroyed in Kharkov and so was the second, modified prototype built under the designation I-360 or the Su-3. The main designer was P. D. Grušin, originally had this machine propel powerful engine M-106, but because this engine was still available, had to be used the power unit from the older Su-1 – engine the Klimov M-105P the turbocharged a pair of turbo-compressors TK-2. One major difference between the two aircraft, however, was in the wings – the Su-3 had a reduced wingspan and was about 2 m2 reduced supporting area. Other changes were in the coolers of water and oil and in their kapotování. Sukhoi Su-3 was not a very successful machine, the turbocompressors were not reliable and if he flew with disconnected turbocompressors, then was the performance of the aeroplane rather below average. After a couple of carried out test years terminated.
sources:
Vladimir Antonov, Yefim Gordon and others, OKB Sukhoi, Leicester, Midland, 1996, ISBN 1-85780-012-5
Vaclav Nemecek, Military aircraft 3 part, the second supplemented edition, Our Troops, Prague 1992, ISBN 80-206-0117-1
http://www.sukhoi.org/planes/museum/su1_3/
http://www.airwar.ru/enc/fww2/su3.html.
In 1941, the kharkov aviation plant had to move to the city of Novosibirsk, the prototype Su-1 was destroyed in Kharkov and so was the second, modified prototype built under the designation I-360 or the Su-3. The main designer was P. D. Grušin, originally had this machine propel powerful engine M-106, but because this engine was still available, had to be used the power unit from the older Su-1 – engine the Klimov M-105P the turbocharged a pair of turbo-compressors TK-2. One major difference between the two aircraft, however, was in the wings – the Su-3 had a reduced wingspan and was about 2 m2 reduced supporting area. Other changes were in the coolers of water and oil and in their kapotování. Sukhoi Su-3 was not a very successful machine, the turbocompressors were not reliable and if he flew with disconnected turbocompressors, then was the performance of the aeroplane rather below average. After a couple of carried out test years terminated.
sources:
Vladimir Antonov, Yefim Gordon and others, OKB Sukhoi, Leicester, Midland, 1996, ISBN 1-85780-012-5
Vaclav Nemecek, Military aircraft 3 part, the second supplemented edition, Our Troops, Prague 1992, ISBN 80-206-0117-1
http://www.sukhoi.org/planes/museum/su1_3/
http://www.airwar.ru/enc/fww2/su3.html.
URL : https://www.valka.cz/Suchoj-Su-3-t724#459860Version : 0
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Reklama
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(Suchoj.com)
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(Suchoj.com)
URL : https://www.valka.cz/Suchoj-Su-3-t724#21605Version : 0
Martin Smíšek
MOD
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Mám ještě jednu fotografii
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URL : https://www.valka.cz/Suchoj-Su-3-t724#116377Version : 0
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