High Temperature (800 to 1600 F) Magnetic Materials
Evaluation of Solid Propellant Rocket Motor Nozzles and Cases
Cryogenic Tensile Properties of Selected Aerospace Materials
Research on New or Improved Liquid Propellants (Fuels, Oxidizers, Monopropellants)
Research on New or Improved Liquid Propellants (U). (Fuels, Oxidizers, Monopropellants)