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March 1965 |
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May 1965 |
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September 1965 |
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March 1966 |
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April 1966 |
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May 1966 |
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September 1966 |
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Construction: | Titanium (Beta-120/Ti-13V-11Cr-3A1)
Monococque with some super-high-temperature plastics. |
Titanium (Beta-120/Ti-13V-11Cr-3A1)
Monococque with some super-high-temperature plastics. |
Length: | 42 ft 10 in | 102 ft 3 in |
Height: | 7 ft 1/4 in | 18 ft 6 in |
Wingspan: | 19 ft 1/4 in | 55 ft 7 in |
Wing Area: | 1,795 square feet | |
Maximum take-off weight: | 11,000 pounds | 117,000 pounds |
Maximum Speed: | 3.35 M | 3.2 M |
Armament: | - | - |
Ceiling: | 95,000 ft | 85,000 ft |
Powerplant: | Marquardt RJ43-MA-11 Ramjet with 1,500 pounds thrust | 2x Pratt & Whitney J75 with
17,000 pounds thrust each (test flights) 2x Pratt & Whitney J58 (JT11D-20A) high-bypass ratio turbojets with 20,500 pounds thrust each |
Production: | 38 | 15 |
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