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Pressure Time History for TP3015 from
Fourier Spectrum of TP3016 from El Stage I
Fourier Spectrum of CM101A from El Stage I
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accelerometer aerodynamic forces Attach Point Left BOOSTER MODELS E-l Burnout With Front Centaur CM101A Flight Data Comparison of CM101A damping ratio Decaying Sine degree of freedom domain solutions Due To Strut E-4 Mode E-l Stage eigenvectors equation 28 equations of motion external forces Figure 67 Flight Data Spectrum Forward Attach Point Fourier Spectrum frequency domain Front and End Helios History for TP3016 Impedance Analytical Predictions impedance technique input frequencies interface accelerations interface forces Landing Due LDEF Left Hand Side Longitudinal Payload Impedance low frequency environment modal damping mode shapes MODELS E-l E-2 Nyquist frequency Point Left Hand Pressure Time History Response At Forward shown in Figures Shuttle Transportation System Side For Landing Side For Lift-Off Slosh Wt spectra Spectrum of CM101A Spectrum of TP3015 Spectrum With Impedance Stage I Burnout Stage I Ox Stage II Fuel Strut Forces tion Titan III transfer characteristics Tukey window