Publisher : The Korean Society for Aeronautical & Space Sciences
DOI : 10.5139/IJASS.2010.11.1.049
Title & Authors
Shock Response Prediction of a Low Altitude Earth Observation Satellite During Launch Vehicle Separation Lee, Dae-Oen; Han, Jae-Hung; Jang, Hae-Won; Woo, Sung-Hyun; Kim, Kyung-Won;
Several pyrotechnic devices are employed over the course of satellite`s missions, generally for the separation of structural subsystems and deployment of appendages. Firing of pyrotechnic devices results in impulsive loads characterized by high peak acceleration and high frequency content which can cause failures of various flight hardware elements and small components. Thus, accurate prediction of acceleration level in various components of spacecraft due to pyrotechnic devices is important. In this paper, two methods for pyroshock prediction, an empirical model and statistical energy analysis in conjunction with virtual mode synthesis, are applied to predict shock response of a low altitude earth observation satellite during launch vehicle separation. The predicted results are then evaluated through comparison with the shock test results.
Pyroshock;Shock Response Spectrum;Statistical Energy Analysis;Virtual Mode Synthesis and Simulation;
A correlation study of satellite finite element model for coupled load analysis using transmissibility with modified correlation measures, Aerospace Science and Technology, 2014, 33, 1, 82
COMS Shock Test Assessment by Using the Extrapolation Method, Journal of the Korean Society for Aeronautical & Space Sciences, 2012, 40, 5, 439
Review of pyroshock wave measurement and simulation for space systems, Measurement, 2012, 45, 4, 631
Pyroshock Prediction of Ridge-Cut Explosive Bolts Using Hydrocodes, Shock and Vibration, 2016, 2016, 1
Mulville, D.R., 1999, Pyroshock Test Criteria, National Aeronautics and Space Administration.
Irvine, T., 2002, An Introduction to the Shock Response Spectrum, Vibrationdata.com.
Baumann, R.C., 1996, General Environmental Verification Specification For STS& ELV Payloads, Subsystems, and Components, NASA Goddard Space Flight Center.
Himelblau, H. et al., 2001, Dynamic Environmental Criteria, National Aeronautics and Space Administration.
Lyon, R.H. and Dejong, R.G., 1998, Theory and Application of Statistical Energy Analysis (2nd edition), RH Lyon Corp., Cambridge.
Dalton, E., and Chambers, B., 1995, “Analysis and Validation Testing of Impulsive load Response in Complex, Multi-Compartmented Structures”, Proceedings of the 36th AIAA Structures, Structural Dynamics, and Materials Conference.
VA One 2008 Shock Module User's Guide and Theory, 2008, ESI Group.