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DESCRIPTION OF ROCKET MOTOR AND TEST
1 Vickers1 SITVC System and EM 72 Rocket
INITIAL THEORETICAL ANALYSIS
16 other sections not shown
Allegany Ballistics Laboratory analysis axial thrust bow shock calculated downstream electronic amplifier EM72 motor equation exit plane exit pressure experimental Fapp flow conditions fluid mechanism Force Ratio Versus frequency modulated Frequency Response full flow Inj ection injection angle injection port Injector Chamber Pressure input program input signal instrumented side Load Cell magnification factor mass flow Measured Side Force motor axis motor nozzle nozzle wall null parameters phase angle Pitch poppet primary nozzle Ratio Versus Flow rocket motor secondary injection nozzles secondary injection system Section sectors Shock Apex shock azimuth shock patterns shock structure shown in Figure Single axis injection solid propellant sonic injection specific impulse ratio speed channels spool supersonic injection Table test data test stand Theoretical Side Force Theoretical Versus Measured Thrust Augmentation thrust vector control transducer transfer function TVC firing TVC test upstream Versus Flow Ratio Versus Measured Side Vickers Visicorder traces Yaw Yaw Yaw