Win View―software for analysis of launch vehicle vibration, acoustics and shock data

摘要

Vibration, acoustics and shock data recorded during flight of PSLV and GSLV launch vehicles has to be analysed for peak, rms, frequency, psd, octave band analysis and SRS in order to obtain the levels experienced during the flight. These levels are required to evaluate the performance of various stages, update the finite element model and to update the environmental test specifications. This analysis software developed using Visual Basic 6 and Visual C++ is tuned to meet flight data analysis requirements.