Axial Force [N] 335.7 168.9 Shear Force [N] -43.0 -21.6 Center of Pressure [% length] 40.0 40.0 Coefficient of Drag CD 1.44 0.81 Dynamic Pressure [Pa] 240 CD % error [%] 63 21 (Jayme Zott) References: 1Sutton, George P., and Oscar Biblarz. Rocket Propulsion Elements. New York: John Wiley & Sons, Inc., 2001. 2The Martin Company, Vanguard Satellite Launching Vehicle”, Engineering Report No. 11022, April 1960. “The
Axial Force [N] Shear Force [N] Center of Pressure [% length] Coefficient of Drag CD Dynamic Pressure [Pa] CD % error [%] 335.7 -43.0 40.0 1.44 63 168.9 -21.6 40.0 0.81 240 21 (Jayme Zott) References: 1Sutton, George P., and Oscar Biblarz. Rocket Propulsion Elements. New York: John Wiley & Sons, Inc., 2001. 2The Martin Company, “The Vanguard Satellite Launching Vehicle”, Engineering Report No. 11022, April 1960.
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