This paper discusses the US Air Force/Bell Aircraft Corporation X-2 project which began in 1945. It was aimed at developing a research aircraft designed to reach speeds of over Mach 3 and altitudes over 100,000ft. A brief description of the aircraft is given along with a discussion of its flight test programme. The much-delayed project ended on 27 September 1956 during the aircraft's 13th powered flight. Loss of control at over Mach 3 led to violent motions characteristic of inertia roll coupling, following which both pilot and aircraft were lost. The paper concludes with an examination of the limited achievements of the project and lessons learned from it.
Lessons Learned from the Bell X-2 Program
Sae Technical Papers
World Aviation Congress & Exposition ; 1997
1997-10-01
Conference paper
English
Lessons learned from the Bell X-2 program
AIAA | 1997
|Lessons Learned from the Bell X-2 Program
British Library Conference Proceedings | 1997
|THE BELL APT UAS FAILSAFE SYSTEM FLIGHT TEST LESSONS LEARNED
TIBKAT | 2023
|