An Aerodynamic Analysis of Saturn I, Block I Flight Test VehiclesNational Aeronautics and Space Administration, 1964 - 57 pages |
Expressions et termes fréquents
0-25 psia Servonics 3.2 Mach Number 30 Error Margin 45 degree flare AMBIENT PRESSURE VERSUS axial force coefficient center of pressure COEFFICIENT VERSUS LONGITUDINAL COEFFICIENT VERSUS MACH Data Estimated 30 Drag Coefficient dynamic pressure error bands Estimated 30 Error Flight Evaluation Flight results FLIGHT TEST VEHICLES fluctuating pressure data Gimbal I-beam fairing interstage area Jupiter nose cone kg/cm² Mach Number FIGURE mass flow rates maximum Meas NASA TN noise measurements normal force observed at Mach Power Spectral Density predicted values PRESSURE COEFFICIENT VERSUS pressure location pressure measurements PRESSURE TO AMBIENT PRESSURE VERSUS MACH RATIO OF SURFACE root-mean-square SA-1 through SA-4 SA-4 INTERSTAGE SA-4 Telemetered Data Saturn flights SATURN I BLOCK Sound Pressure Level steady-state pressures strain gauge Surface Pressure Coefficient Surface Pressure/Ambient Pressure Telemetered Data Estimated telemetry Test Data Ref trajectory Tunnel Test Data vehicles SA-1 VERSUS LONGITUDINAL STATION VERSUS MACH NUMBER wind tunnel data Wind Tunnel Test