Fast burning rates in thin film propellants
Fast burning rates in thin film solid composite propellants composed of McCormick-Selph 510, 164 monopropellant, oxidizer and polyvinyl chloride binder
Rodenberger, C. A.↗
Engineering topics
Sawyer, M. L.
Publications and source records attributed to Sawyer, M. L..
Feasibility of obtaining hypervelocity acceleration using propellant lined launch tubes Final report, 27 Sep. 1966 - 5 May 1970
Feasibility of explosive lining in launch tube for hypervelocity projectile acceleration
Rodenberger, C.↗