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STATIC AERODYNAMIC CHARACTERISTIC OF A THREE -STAGE ROCKET VEHICLE HAVING VARIOUS FIN CONFIGURATIONS AT LOW SUBSONIC MACH NUMBERS AND ANGLES OF ATTACK UP TO 28(DEGREE)

By: Brown,Clarence A.
Contributor(s): Putnam,Lawrence E.
Material type: materialTypeLabelBookSeries: NASA Technical Note. Publisher: NASA, Washington, D.C. 1963Description: 26p.Subject(s): Aerospace
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