Static stability and drag characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0 /
J.T. Best, Jr. and R.W. Rhudy.

APA Citation

Best, J. T., Rhudy, R. W.., ARO, I., Arnold Engineering Development Center., United States. Air Force. Systems Command. (1974). Static stability and drag characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0. Arnold Air Force Base, Tennessee: Arnold Engineering Development Center, Air Force Systems Command, United States Air Force.

MLA Citation

United States. Air Force. Systems Command, et al.. Static Stability And Drag Characteristics of the HAST Missile At Mach Numbers 2.25, 3.0, And 4.0. Arnold Air Force Base, Tennessee: Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974.