| 词条 | Chizhevski BOK-1 | |||||||||||||||
| 释义 |
The BOK-1 (Byuro Osobykh Konstrooktsiy - bureau of special design), (a.k.a. SS (Stratosfernii Samolyet – stratospheric aircraft)), was an experimental high-altitude aircraft designed and built in the USSR from {{avyear|1934}}. DevelopmentThe BOK was formed as part of TsAGI (Tsentrahl'nyy Aerodinamicheskiy i Ghidrodinamicheskiy Institoot- central aerodynamics and hydrodynamics institute) on the orders of the Soviet Revolutionary Military Council in Dec {{avyear|1930}}. One of the first tasks of BOK was to design and build the hermetically sealed gondola of the SSSR-1 high-altitude balloon. BOK engineers were sent to the Junkers factory at Dessau to study the Junkers Ju 49 which was the first aircraft fitted with a sealed cabin for high-altitude flight. The gondola for the SSSR-1 was designed, built and flown successfully to an altitude of 18,000m in {{avyear|1933}}. The BOK was then assigned the task of applying the 'hermetic' cabin to an aircraft with the Tupolev RD chosen as the basis of the BOK-1. A sealed 1.8 m3 cylindrical cabin constructed from 1.8-2mm D1 light alloy was fitted to a modified RD airframe. The cabin had convex bulkheads front and rear with the main entry hatch in the roof and emergency exit through a porthole at the rear. Seven portholes gave sufficient vision with five for the pilot and two for the radio operator/observer. A maximum design pressure differential of 0.22 kg/cm2 (3.2 lb/in2) held the cabin altitude at 8,000m (26,250 ft) up to the aircraft ceiling of 14,000 m (46,260 ft). With the cabin structure sealed, cabin air was dumped overboard at a controlled rate through a dump valve and replaced with oxygen, from storage bottles, maintaining oxygen levels roughly constant. Heating was supplied through radiators in the engine cooling circuit, to keep the cabin between 15 and 18 °C. The RD airframe was modified with reduced span wings, restressed structure for lower gross weight, fixed spatted single mainwheels, an M-34RN engine and three-bladed propeller, and later an M-34RNV engine and four-bladed propeller. Built at GAZ-35 the BOK-1 was first flown by I.F. Petrov in the summer of 1936 and reached a maximum altitude of 14,000 m in {{avyear|1938}}. Variants
Specifications (BOK-1 M-34RNV){{aerospecs|ref= Gunston, Bill. “The Osprey Encyclopaedia of Russian Aircraft 1875–1995”. London, Osprey. 1995. {{ISBN|1-85532-405-9}} |met or eng?=met |crew= 2 |capacity= |length m= 12.86 |length ft= 42 |length in= 2½ |span m= 30 |span ft= 98 |span in= 5 |swept m= |swept ft= |swept in= |rot number= |rot dia m= |rot dia ft= |rot dia in= |dia m= |dia ft= |dia in= |width m= |width ft= |width in= |height m= |height ft= |height in= |wing area sqm= 78.8 |wing area sqft= 848 |swept area sqm= |swept area sqft= |rot area sqm= |rot area sqft= |volume m3= |volume ft3= |aspect ratio= |wing profile= |empty weight kg= 3,600 |empty weight lb= 7,937 |gross weight kg= 4,800 |gross weight lb= 10,582 |lift kg= |lift lb= |eng1 number= 1 |eng1 type= M-34 RNV |eng1 kw= 619 |eng1 hp= 830 |eng1 kn= |eng1 lbf= |eng1 kn-ab= |eng1 lbf-ab= |eng2 number= |eng2 type= |eng2 kw= |eng2 hp= |eng2 kn= |eng2 lbf= |eng2 kn-ab= |eng2 lbf-ab= |max speed kmh= 260 |max speed mph= 162 |max speed mach= |cruise speed kmh= |cruise speed mph= |stall speed kmh= |stall speed mph= |range km= |range miles= |endurance h= 4 |endurance min= |ceiling m= 14,100 |ceiling ft= 46,260 |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |sink rate ms= |sink rate ftmin= |armament1= |armament2= |armament3= |armament4= |armament5= |armament6= }} See also{{aircontent|see also= |related= |similar aircraft=
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}} References{{refbegin}}
2 : Soviet experimental aircraft 1930–1939|Germany–Soviet Union relations |
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