Specifications
| Type | two-crew supersonic strategic heavy bomber prototype |
| Contractor | North American |
| Country of Origin | USA |
| Powerplant | six General Electric YJ93-GE-3 turbojet engines |
| Thrust | 28,000lbs reheated each |
| Length | 185ft 8in |
| Height | 30ft |
| Wingspan | 105ft |
| Wing Area | 6,297 Sq. ft |
| Max Speed | 1,980mph (mach 3+) @ optimum altitude |
| Climb Rate | 7,170ft/minute |
| Service Ceiling | 75,500ft |
| Range | 3,417 miles |
| Empty Weight | 231,215lbs |
| Max Take-Off Weight | 521,056lbs |
| Armament |
