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Rockwell YB-1A 'Lancer'
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Description
|   Manufacturer: | Rockwell |
|   Base model: | B-1 |
|   Designation: | YB-1 |
|   Version: | A |
|   Nickname: | Lancer |
|   Designation System: | U.S. Tri-Service |
|   Designation Period: | 1962-Present |
|   Basic role: | Bomber |
|   Status: | Prototype |
|   First Flew: | 1974/12/23 |
Specifications
|   Length: | 150 2" | 3.8 m |
|   Height: | 33' 7" | 10.2 m |
|   Wingspan: | 136' 8" | 41.6 m |
|   Gross Weight: | 389,000 lb | 176,417 kg |
Propulsion
|   No. of Engines: | 4 |
|   Powerplant: | General Electric F101-GE-100 |
|   Thrust (each): | 30,000 lb | 13,605 kg |
Performance
|   Cruise Speed: | 647 mph | 1,041 km/h | 562 kt |
|   Max Speed: | 1,390 mph | 2,238 km/h | 1,209 kt |
|   Ceiling: | 60,000 ft | 18,287 m |
 
Recent comments by our visitors
dave houle , CA | was this the one that crashed at EAFB/ wing sweep was involved I believe/ Anyone have any details of that accident? 11/01/2000 @ 00:54 [ref: 974] |
 
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