Crash Site of Chuck Yeager's NF-104A
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The aircraft was destroyed in the ensuing crash on December 10, 1963. An investigation later showed that the cause of the crash was a spin that resulted from excessive angle of attack and lack of aircraft response. The excessive angle of attack was not caused by pilot input but by a gyroscopic condition set up by the J79 engine spooling after shut down for the rocket-powered zoom climb phase. www.chuckyeager.com/home.htm
“On December 10, 1963, while testing an NF-104A rocket-augmented aerospace trainer, he narrowly escaped death when his aircraft went out of control at 108,700 feet (nearly 21 miles up) and crashed. He parachuted to safety at 8,500 feet after vainly battling to gain control of the powerless, rapidly falling craft. In this incident he became the first pilot to make an emergency ejection in the full pressure suit needed for high altitude flights.” (from the biography of Gen. Yeager)
“On December 10, 1963, while testing an NF-104A rocket-augmented aerospace trainer, he narrowly escaped death when his aircraft went out of control at 108,700 feet (nearly 21 miles up) and crashed. He parachuted to safety at 8,500 feet after vainly battling to gain control of the powerless, rapidly falling craft. In this incident he became the first pilot to make an emergency ejection in the full pressure suit needed for high altitude flights.” (from the biography of Gen. Yeager)
Wikipedia article: http://en.wikipedia.org/wiki/NF-104A
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Coordinates: 35°7'25"N 118°8'50"W
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