Allik, ViljoTilk, TeetVendt, RihoAllik, MariTartu Ülikool. Loodus- ja täppisteaduste valdkondTartu Ülikool. Tehnoloogiainstituut2016-06-152016-06-152016http://hdl.handle.net/10062/51868Components used in space are subject to high frequency and high amplitude mechanical shocks that occur during the launch and separation phases of the space vehicles. Shock testing is done to ensure that components can withstand the shock events. A shock can be described by an acceleration and time history, but in shock testing it is difficult to manage and quantify shocks by only looking at the acceleration and time history of a shock. Instead, a shock response spectrum is used, which plots the peak accelerations of multiple single degree of freedom systems with their own unique frequencies over a range of frequencies, usually from 100 Hz to 10 000 Hz. The shocks that occur in space can reach up to acceleration levels of 10 000 g’s. The main objective of this work was to develop a software application for the mechanical shock testing system at Tartu Observatory. The shock testing system at Tartu Observatory consists of a resonant plate, pendulum hammer, guiding rod, weights and a data acquisition module with acceleration sensors. The software was developed in Microsoft Visual Studio .NET 2003 using the C++ programming language and external libraries. The software is required to acquire the data from the sensors connected to the data acquisition module and process and plot it. The shock response spectrum and acceleration-time histories can be plotted. An important aspect of shock testing is to be able to recreate shocks of various levels. If the shock testing system manages to do this, the system is considered reliable. To test the reliability of the system, the developed software was tested by performing shock testing on test objects and plotting the results.engShock testing, shock response spectrum, signal processing, data acquisitonmagistritöödThesis