More about Martin T. Moul:
| | Books by Martin T. Moul: Books in the extended shelves: Moul, Martin T.: Dynamic stability and control problems of piloted reentry from lunar missions (National Aeronautics and Space Administration, 1961), also by James L. Williams and Albert A. Schy (page images at HathiTrust) Moul, Martin T.: Flight investigation of a supersonic canard missile equipped with an auxiliary damping-in-pitch control system (Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953), also by United States National Advisory Committee for Aeronautics and Langley Aeronautical Laboratory (page images at HathiTrust) Moul, Martin T.: Longitudinal stability and control characteristics from a flight investigation of a cruciform canard missile configuration having an exposed wing-canard area ratio of 16:1 (National Advisory Committee for Aeronautics, 1952), also by Andrew R. Wineman, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
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