Foward Swept Wing Aircraft PAGE
2005 / 1 / 5 Update.
ITARR-TASS/Aviapanorama |
Sukhoi S-37 Foward Swept Wing Experimental Aircraft Length : 22.6m
Wing Span : 16.7m Hight : 6.4m All-Up Weight : 34,000Kg Empty Weight : 25,760Kg Engine : Aviadvigatel D-30F6 Turbojet (15,500Kgf) Max Speed : 2,200Km/h Service Ceiling : 18,000m Max Range : 3,300Km Crew : 1 |
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This Project was Cancelled ! |
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Wing Span: 21.7m Hight : 7.4m Wing Area : 52.3 Sqare Meter All-Up Weight : 17,932Kg Empty Weight : 9,877Kg Engine : Westinghouse J34-WE-22 TurboJet (1,640Kg) X 2 Max Speed : 829m/h Cluse Speed : 676Km/h Max Range : 4,585Km Service Ceiling : 11,735m Crew : 3 |
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| LINK WEB PAGE | ||
| USAF Museum | ||
Rockwell |
Northamerican WS-110A Supersonic Bomber A Prototype of XB-70 Valkyrie. This was Northamerican proposal Design. |
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![]() General Dynamics |
General Dynamics Ploposal. |
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![]() Rockwell International |
Project was Canncelled. But, this project was became X-29 basic design. |
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NASA |
Wing Span : 8.29m Hight : 4.34m Wing Area : 17.54 Square meter All-Up Weight : 7,850Kg Empty Weight : 6,170Kg Engine : General Electric F404-GE-400 Turbofun (7,258Kg) X 1 Max Speed : 1,909Km/h (Mach 1.6) Service Ceiling : 16,760m Crew : 1 |
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