Static aerodynamic characteristics of three-stage trailblazer ii rocket vehicle determined in low turbulence pressure wind tunnel
STATIC AERODYNAMIC CHARACTERISTICS OF A THREE-STAGE ROCKET VEHICLE HAVING VARIOUS FIN CONFIGURATIONS AT LOW SUBSONIC MACH NUMBERS AND ANGLES OF ATTACK UP TO 28 DEG
1963-04-01
Sonstige
Keine Angabe
Englisch
Forebody Strake Effects on Rocket Aerodynamic Characteristics at High Angles of Attack
Online Contents | 2008
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