Accession Number : ADA323344
Title : Shock Trials Trojka Drone; Measurements Shot 4, 5 and 6.
Descriptive Note : Final rept.,
Corporate Author : CENTRE FOR MECHANICAL ENGINEERING TNO DELFT (NETHERLANDS)
Personal Author(s) : Bosman, B.
PDF Url : ADA323344
Report Date : 02 JAN 1997
Pagination or Media Count : 224
Abstract : In the scope of the development of the Trojka drone a test structure has been subjected to 2 series of 3 underwater shock loads of increasing shock levels. During these tests TNO carried out measurements with 24 strain gauges, 28 accelerometers, 4 relative displacement transducers and 2 pressure transducers. This report presents the measured pressure signals, strain signals, relative displacements, accelerations, the calculated maximax shock response spectra (at 1% damping) and, by integration of the accelerations, velocities and displacements, of the second series of 3 measurements.
Descriptors : *SHOCK RESISTANCE, *DRONES, *UNDERWATER EXPLOSIONS, ACCELEROMETERS, NETHERLANDS, PRESSURE TRANSDUCERS, SHOCK WAVES, DAMAGE ASSESSMENT, OPERATIONAL EFFECTIVENESS, EXPLOSION EFFECTS, IMPACT SHOCK, STRUCTURAL RESPONSE, STRAIN GAGES, TABLES(DATA), SHOCK TESTS, REMOTE CONTROL, UNDERWATER SOUND SIGNALS, EXPLOSION BUBBLES, ACOUSTIC MINESWEEPING, SHOCK SPECTRA, STRUCTURAL INTEGRITY.
Subject Categories : Marine Engineering
Distribution Statement : APPROVED FOR PUBLIC RELEASE