R. W. Cubbison

Supersonic aerodynamic heating tests on a lightweight external insulation system for liquid-hydrogen tanks of boost vehicles

R. P. Cochran, R. W. Cubbison, 1966 .

Performance characteristics from Mach 2.58 to 1.98 of an axisymmetric mixed-compression inlet system with 60-percent internal contraction

R. W. Cubbison, D. F. Johnson, E. T. Meleason, 1969 .

Effect of bleed-system back pressure and porous area on the performance of an axisymmetric mixed-compression inlet at Mach 2.50

R. W. Cubbison, B. W. Sanders, 1968 .

Performance of several half-conical side inlets at supersonic and subsonic speeds

L. E. Stitt, R. J. Flaherty, R. W. Cubbison, 1956 .

Thrust and direction control apparatus Patent

J. F. Connors, R. W. Cubbison, 1966 .

Effect of porous bleed in a high performance axisymmetric, mixed compression inlet at Mach 2.50

R. W. Cubbison, D. F. Johnson, E. T. Meleason, 1968 .