Aerodynamic characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0 /
J.H. Jones.
APA Citation
Jones, J. H.., ARO, I., Arnold Engineering Development Center., United States. Air Force. Systems Command. (1972). Aerodynamic 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
Jones, J. H., Inc. ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command. Aerodynamic 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, 1972.
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