Axial Force [N] 486.9 298.1 Shear Force [N] -99.4 -60.8 Center of Pressure [% length] 38.3 38.3 Coefficient of Drag CD 1.38 0.85 Dynamic Pressure [Pa] 279 CD % error [%] 54 17 (Jayme Zott) References 1Sutton, George P., and 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 [%] 486.9 -99.4 38.3 1.38 54 298.1 -60.8 38.3 0.85 279 17 (Jayme Zott) References 1Sutton, George P., and 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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