1970•NASA Technical Reports Server (NASA)Requires access

Feasibility of obtaining hypervelocity acceleration using propellant lined launch tubes Final report, 27 Sep. 1966 - 5 May 1970

CHARLES A. RODENBERGER, Miriam Sawyer, M.M. Tower

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Key concepts: Hypervelocity, Propellant, Acceleration, Aerospace engineering, Aeronautics, Physics, Environmental science, Nuclear engineering

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Feasibility of obtaining hypervelocity acceleration using propellant lined launch tubes Final report, 27 Sep. 1966 - 5 May 1970 — Research Paper | ScholarLens