Research Article  Open Access
YongWoon Kim, JaeKyeong Jang, JungRyul Lee, HakSeong Gim, "Hybrid Method of Modal Analysis and Laser Shock Scanning to Visualize the Pyroshock Propagation in a Tension Joint", Shock and Vibration, vol. 2019, Article ID 4389595, 13 pages, 2019. https://doi.org/10.1155/2019/4389595
Hybrid Method of Modal Analysis and Laser Shock Scanning to Visualize the Pyroshock Propagation in a Tension Joint
Abstract
The use of pyrodevices in the aerospace industry has been increasing because of their ability to implement separation missions with a small weight, for example, space launchers, spacecrafts, and missiles. During operation, pyrodevices generate pyroshock, which causes failures of electronic devices. Recently, a pyroshock simulation method using laser shock has been developed to evaluate the risk of pyroshock before flight mission. However, depending on the structure, the laser shock showed some difficulty simulating pyroshock in the lowfrequency regime accompanying vibration. Therefore, in this study, we developed a hybrid method of numerical modal analysis and laser shockbased experimental simulation to visualize the pyroshock propagation in all the relevant frequency regimes. For the proof of concept of the proposed method, we performed experiments of explosive boltinduced shock and pyrolockinduced shock in the openboxtype tension joint and compared the hybrid simulation results with actual pyroshock. From the results, we obtained the simulated timedomain signal with an averaged peaktopeak acceleration difference (PAD) of 11.2% and the shock response spectrum (SRS) with an averaged mean acceleration difference (MAD) of 28.5%. In addition, we were able to visualize the simulation results in the temporal and spectral domains to compare the pyroshock induced by each pyrodevice. A comparison of the simulations showed that the pyrolock had an impulse level of 1/12 compared to the explosion bolt. In particular, it was confirmed that the pyrolockinduced shock at the near field can cause damage to the electronic equipment despite a smaller impulse than that of the explosive boltinduced shock. The hybrid method developed in this paper demonstrates that it is possible to simulate pyroshock for all the frequency regimes in complex specimens and to evaluate the risk in the time and frequency domain.
1. Introduction
Pyrodevices separate a substructure from a main structure via an explosion. Pyrodevices are widely used in the aerospace field because they have the advantages of enabling a separation mission with low weight and small volume [1, 2]. However, during operation, such a pyrodevice generates a highfrequency pyroshock, which causes failures in electronic devices [3]. According to a NASA technical memorandum published in 1988, 84 failures related with pyroshock occurred during 600 missile missions over 23 years, most of which were caused from the shock above 3 kHz [4]. Therefore, it is necessary to study the pyroshock to ensure the safety of the mission.
Pyroshock is divided into pointsource pyroshock, linearsource pyroshock, and combinedsource pyroshock, depending on the type of the pyrodevice. In addition, pyroshock is divided into three fields according to the magnitude and frequency of the response [5–7]. Figure 1 shows the pyroshock classification criteria. As shown in Figure 1, because the pyroshock includes broadfrequency band components, it is necessary to quantify the characteristics and risk of each. The most widely used quantification technique is the shock response spectrum (SRS), which is calculated based on the acceleration time history of pyroshock [8, 9].
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Various simulation techniques have been developed to study pyroshock. Although there have been studies to simulate pyroshock using mechanical shocks, they all have limitations in that they can only be simulated for pointsource pyroshock [10, 11]. In addition, finite element analysis has been used to simulate pyroshock in the lowfrequency regime such as the far field. However, the finite element models used were not accurate for numerical simulation of the highfrequency structural response [12, 13]. Recently, research has involved simulation of pyroshock experimentally using laser shock. In this simulation approach, when the laser is irradiated onto the specimen, a thermal shock is generated via the thermoelastic mechanism, resulting in instant thermal expansion. These laser shocks contain a broad range of frequency components that were reported to be suitable for simulating pyroshock up to the highfrequency regime, such as those in the mid field and near field. In fact, various cases of pyroshock have been simulated using laser shock training based on an iterative signal decomposition and synthesis method [14]. However, this technique often showed low estimation accuracy in the lowfrequency regime of subkilohertz frequencies, which might accompany engineering vibration, because the laser pulseinduced elastic wave contains primarily highfrequency components. In other words, laser shockbased simulation of the pyroshock accompanying subkilohertz vibration is very challenging to perform because of the structural boundary condition.
To overcome these limitations described above, we developed a hybrid method of modal analysis and laser shock scanning to simulate the pyroshock over the whole frequency regime. In the far field, with lowfrequency components less than 3 kHz, because the finite element analysis verified the accurate simulation performance [12, 13], the farfield pyroshock was simulated using the modal analysis. In the mid and near field, because the laser shockbased experimental simulation provided accurate simulation performance [14], the mid and nearfield pyroshock over 3 kHz was simulated using laser shock. Each simulation result was superimposed and reconstructed to the pyroshock based on iterative signal decomposition and synthesis. In this study, the acceleration time history of pyroshock and the SRS are simulated. The simulation results are compared to actual pyroshock. A peaktopeak acceleration difference (PAD) and a mean acceleration difference (MAD) are used to determine the similarity between the simulation results and the actual pyroshock. The PAD represents the error of the peaktopeak response of the timedomain signal, and the MAD represents the error of the SRS between simulated results and the actual pyroshock [14]. There are other statistical measures which are commonly used to compare the similarity between signals such as correlation coefficient or root mean square deviation [15, 16]. However, in the pyroshock study, the similarity of the peaktopeak acceleration is more important than the similarity of the whole signal in simulation of the timedomain signal.
The hybrid method developed in this study proves that the pyroshock can be simulated in a complex structure, such as an openboxtype tension joint; thus, the method can be used to evaluate the risk of pyroshock in the temporal and spectral domains.
2. Pyroshock Simulation Using the Hybrid Method of Modal Analysis and Laser Shock Scanning
Figure 2 shows the flow chart of the pyroshock simulation algorithm developed in this study. The algorithm is comprised of six steps. In the first step, actual pyroshock signals are measured using laser Doppler vibrometers (LDVs). In the second step, laser shock signals generated by a Qswitched laser are acquired through a broadband PZT sensor in a wave propagation imaging system (GUPI, XNDT Inc.). In the third step, modal analysis is performed on the subkilohertz vibration regime, often called the far field, even though the distance from the source is not far, and then the result is superimposed on the laser scanning data and stored as reference data. In the fourth step, the difference between the reference data and the actual pyroshock is analyzed based on the SRS, and then, the optimized gain value for correcting the difference between the two signals is selected and applied to predict the SRS of pyroshock. In the fifth step, the information of the predicted SRS is given to the laser scanning data using an iterative signal decomposition and synthesis method developed in [14] to simulate the timedomain signal of the pyroshock at all the scan areas. In the final step, the pyroshock wave propagation image (PWPI) and the shock response spectrum image (SRSI) are obtained using simulated pyroshock signals and spectra, respectively.
2.1. Pyroshock Measurement on an OpenBoxType Tension Joint
A 1/2inch explosive bolt (Hanwha Corporation), shown in Figure 3(a), is a conventional pyrodevice, which is separated by a ridgecut mechanism [17]. The explosive bolts have advantages of simple operation and low weight, but they have the disadvantage of providing a large impulse. Figure 3(b) is a pyrolock device (Hanwha Corporation) designed to reduce the impulse of the explosive bolts. In this study, we used the developed hybrid method to simulate the explosive boltinduced shock and the pyrolockinduced shock and then compared them in time and frequency domains. In the experiment, an openboxtype tension joint made of a stainlesssteel material was used to simulate the environment in which the substructure is separated from the main structure. The openboxtension joint has four surfaces with one free edge where considerable vibration is also induced via explosion. Two types of pyrodevices were installed on the specimens, and pyroshock signals were measured using three LDVs. Details of the measurement point and test specimens are shown in Figure 3(c). The coordinates of the measurement points are represented by . The voltage signals collected from the LDVs are stored in the PC, where the pyroshock voltage signal is denoted by . is then converted to the pyroshock signal, , of the acceleration unit through a conversion process using equation (1). The detailed conditions of data acquisition are listed in Table 1:where is the pyroshock signal of digital voltage form (V), is the pyroshock signal of the acceleration unit (g), is the calibration factor of LDV, is the attenuation factor of the attenuator, and is the measurement unit of the LDV sensor (m/s/V).
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2.2. Laser Shock Scanning Measurement on the OpenBoxType Tension Joint
Through the pyroshock measurement process, we can observe the characteristics of the pyroshock. However, the point measurement of the actual pyroshock at limited points is not sufficient to understand and analyze the pyroshock that is propagated over the structure. To visualize the propagation of pyroshock in the full field over the structure, we simulate pyroshock using laser shock. The same structure used in the pyroshock measurement was prepared to obtain the laser shock signals. Next, PZT sensors were installed in place of the pyrodevice, as shown in Figure 4, because the reciprocal setup of the laser shock scanning system with a wavelength of 532 nm (GUPI, XNDT Inc.) designates the sensor locations’ shock source locations. Subsequently, the laser scanning process was performed by setting the signal acquisition conditions through the GUI platform. The laser shocks generated by using the Qswitched laser were collected through a PZT sensor, and the obtained laser scanning data were represented by , depending on the laser shock location. In this case, the scanning area was set to include pyroshock measurement points, as shown in Figure 4. The data acquisition condition of the laser scanning data is shown in Table 2.

2.3. Modal Analysis for the Simulation of Pyroshock on the OpenBoxType Tension Joint
Because the PZT sensor used to acquire laser shock scanning data is a contact type and broadband sensor of a central frequency of 200 kHz and a bandwidth of 1.2 MHz, the sensitivity differs, depending on the frequency range. However, the PZT has poor sensitivity in the subkilohertz regime. The pyroshock simulation requires shock signal acquisition over a very wide frequency range, and the laser shockcapturing sensor requires very high sensitivity; however, it is difficult to find such a widerange PZT sensor covering the whole pyroshock analysis range with high sensitivities over the range. In addition, the LDV is not suitable for the simulation because it provides SNR insufficient for measuring laser shock signal. Therefore, we developed the hybrid method involving the finite element analysis method for the lowfrequency pyroshock accompanying vibration and the laser scanning method in the highfrequency regime, utilizing the advantages of each of the two simulation methods. Figure 5 shows the hybrid simulation process. First, modal analysis is performed on the lowfrequency vibration regime. Figure 5(a) shows the FEM analysis model and the blue surface means fixed condition. The modal analysis results are shown in Figure 5(b). After completing the modal analysis, , expressed by a relative displacement value, is obtained by extracting the result in the interested area. , which is the analysis value at the same point as an arbitrary measurement point of pyroshock, is extracted, and then, the ratio to the is stored in . is a representative gain value for all points that convert the modal analysis result saved as the relative displacement value into the amplitude of the actual pyroshock. By multiplying by , the SRS of the pyroshock corresponding to the highfrequency regime is predicted. is obtained by providing a sine wave to the predicted SRS of the pyroshock in the lowfrequency component as shown in Figure 5(c). Finally, the obtained is superimposed with the laser scanning data to obtain reference data to be used for the pyroshock simulation. Because the openboxtype tension joint used in this experiment was a stainlesssteel material, the modal analysis was performed under the conditions shown in Table 3. In the process of obtaining the gain value, pyroshock signals at the measurement point 3 were used.

2.4. 1/2Inch Explosive BoltInduced Shock Simulation on the OpenBoxType Tension Joint
Using only two sets of pyroshock data, which were measured at point 1 and point 3, a 1/2inch explosive boltinduced pyroshock simulation was performed based on iterative signal decomposition and synthesis. Further information on the iterative signal decomposition and synthesis method can be found in reference [14]. Figure 6 shows the pyroshock simulation results at the training point. The black signal represents the actual pyroshock signal, and the blue signal represents the simulation result. At training point 1, the timedomain signal was simulated with a PAD of 8.77%, and the SRS was simulated with an MAD of 34.03%. At training point 3, the timedomain signal was simulated with a PAD of 14.37% and the SRS was simulated with an MAD of 22.75%. The PWPI and SRSI were obtained as shown in Figure 7 by applying the gain value obtained through the training process to all the points equally. Figure 7(a) shows a snapshot of the PWPI at 300 μs, and Figures 7(b)–7(d) show snapshots of the SRSIs at 1 kHz, 3 kHz, and 30 kHz, respectively. To verify the reliability of the obtained PWPI and SRSI, the simulated results were compared with the actual pyroshock at measurement point 2, which was not used at all in the simulation process. As shown in Figure 8, the comparison results confirmed that the timedomain signal was simulated with a PAD of 4.87%, and the SRS was simulated with an MAD of 31.92%.
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2.5. 1/2Inch PyrolockInduced Shock Simulation on the OpenBoxType Tension Joint
Using only two sets of pyroshock data, which were measured at point 1 and point 3, a 1/2inch explosive boltinduced pyroshock simulation was performed based on iterative signal decomposition and synthesis. Figure 9 shows the pyroshock simulation results at the training point. The black signal represents the actual pyroshock signal, and the blue signal represents the simulation result. At training point 1, the time domain signal was simulated with a PAD of 22.70%, and the SRS was simulated with an MAD of 29.20%. At training point 3, the time domain signal was simulated with a PAD of 3.89%, and the SRS was simulated with an MAD of 29.01%. The PWPI and SRSI were obtained as shown in Figure 10 by applying the gain value obtained through the training process to all the points equally. Figure 10(a) shows a snapshot of PWPI at 300 μs, and Figures 10(b)–10(d) show snapshots of SRSI at 1 kHz, 3 kHz, and 30 kHz, respectively. To verify the reliability of the obtained PWPI and SRSI, the simulated results were compared with the actual pyroshock at measurement point 2, which was not used at all in the simulation process. As shown in Figure 11, the comparison results confirmed that the time domain signal was simulated with a PAD of 12.60%, and the SRS was simulated with an MAD of 24.92%.
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3. Comparison between Explosive BoltInduced Shock and PyrolockInduced Shock Using Simulation Results
Table 4 shows the peaktopeak acceleration of the pyrolock and explosive boltinduced shocks. The pyrolockinduced shock compared to the explosive bolt shows the impulse amount of 1/12 level at measurement points 1 and 3 and 1/5 level at measurement point 2. Because the pyroshock is affected by the geometrical shape of the structure, the impulse ratio of the two pyrodevices differs depending on the measurement point. Therefore, it is difficult to quantitatively evaluate the impulse of pyrolock and explosive bolt based on only the peaktopeak acceleration information at three points. The system developed in this study simulated pyroshock at all points and visualized the pyroshock in the time domain and frequency domain to quantitatively compare the impulse amount of an explosive bolt and a pyrolock. Before comparing the simulation results, we first summarize the similarity between the actual pyroshock and simulation results in Table 5 to verify the simulation results. The timedomain signal was simulated with an averaged PAD of 11.2%, and the SRS was simulated with an averaged MAD of 28.5%. Figure 12 shows that the simulation performance is improved compared to the pyroshock simulation method based on the laser shock developed in the past. Moreover, considering that the repeatability of the pyroshock itself is approximately 20% [14], the simulation performance is satisfactory. Because the reliability of the simulation results was verified, the impulses of an explosive bolt and a pyrolock were analyzed using the simulation results. Figure 13(a) shows the result of visualization of the explosive boltinduced shock in the time domain and frequency domain, and Figure 13(b) shows the visualization of the pyrolockinduced shock in the time domain and frequency domain. Comparing the simulation results in the time domain using the PWPI, the pyrolock is found to have a smaller impulse amount compared to the conventional explosive bolt. Because the timedomain signal is a superposition of various frequency components, it is necessary to confirm which frequency component is reduced. The SRSI is divided into a farfield regime corresponding to 100 Hz to 3 kHz including a lowfrequency vibration component, a midfield regime corresponding to 3 kHz to 10 kHz, and a nearfield regime corresponding to 10 kHz to 100 kHz. In the far field, the two shocks do not show a large difference, whereas in the midfield and nearfield regime, a marked decrease in the amount of pyrolock impulse is found.


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4. Conclusions
In this study, we developed a hybrid method of modal analysis and laser shock scanning to visualize the pyroshock propagation accompanying vibration according to the boundary condition and to evaluate the risk of pyroshock. The hybrid method predicts the characteristics of pyroshock in the openbox tension joint by combining laser shock and modal analysis where the modal analysis was used to superimpose the lowfrequency vibration to pyroshock propagation; Both laser shock and modal analysis results were superposed and reconstructed to the pyroshock using iterative signal decomposition and synthesis. The pyroshock propagation characteristics of the two different pyrodevices, an explosive bolt and a pyrolock, in the openboxtype tension joint were simulated using the developed hybrid simulation method. The timedomain signal was simulated with an averaged PAD of 11.2%, and the SRS was simulated with an averaged MAD of 28.5%. Considering that the repeatability of the pyroshock itself is approximately 20%, the simulation performance was found to be satisfactory. On the contrary, simulation results at point 1 show relatively higher MAD and PAD than the other two points. The reason was that the point 1 showed much more complex response than the other two points since it was the result of measurement near the stiffer boundary. In order to improve the simulation results in this boundary, further investigation of various wave modes seems necessary. We visualized the simulation results in the temporal and spectral domains to compare the pyroshock induced by each pyrodevice. A comparison of the simulations showed that the pyrolock has an impulse level 1/12 in magnitude compared to that of the explosion bolt. In particular, it was confirmed that, in the near field, the pyrolockinduced shock has a smaller impulse magnitude than the explosive boltinduced shock. The hybrid method developed in this paper demonstrated that it is possible to simulate pyroshock over the entire frequency regime in complex specimens accompanying vibration and to evaluate the risk in time and frequency domains.
Data Availability
The data used to support the findings of this study are available from the corresponding author upon request.
Conflicts of Interest
The authors declare that there are no conflicts of interest regarding the publication of this paper.
Acknowledgments
This research was supported by the National Research Foundation of Korea (NRF) Grant funded by the Ministry of Science and ICT (NRF2017R1A5A1015311) and by the research grant (PMD) of the Agency for Defense Development and Defense Acquisition Program Administration of the Korean government.
References
 L. J. Bement, “Pyrotechnic system failures: causes and prevention,” in NASA Technical Memorandum 100633, pp. 1–3, NASA, Washington, DC, USA, 1988. View at: Google Scholar
 E. Fillippi, H. Attouoman, and C. Conti, “Pyroshock simulation using the alcatel etca test facility, in: launch vehicle vibrations,” in Proceedings of the 1st European Conference, pp. 1–3, CNES, Toulouse, France, June 1999. View at: Google Scholar
 L. J. Bement and M. L. Schimmel, “A manual for pyrotechnic design, development and qualification,” in NASA Technical Memorandum, vol. 110–172, p. 3, NASA, Washington, DC, USA, 1995. View at: Google Scholar
 C. J. Moening, “Pyrotechnic shock flight failures,” in Proceedings of the Institute of Environmental Sciences Pryotechnic Shock Tutorial Program, 31st Annual Technical, Meeting, pp. 2–4, Washington, DC, USA, May 1985. View at: Google Scholar
 IESTRPDTE032.2, Pyroshock Testing Techniques, Institute of Environmental Sciences and Technology, Schaumburg, IL, USA, 2011.
 MILSTD810F, Environmental Engineering Considerations and Laboratory Tests, Department of Defense, USA, Pentagon, VA, USA, 2000.
 Anon, “Pyroshock test criteria,” in NASA Technical Standard NASASTD 7003A, p. 15, NASA, Washington, DC, USA, 2011. View at: Google Scholar
 J. E. Alexander, “Shock response spectrum a primer,” Sound and Vibration, vol. 43, pp. 6–14, 2009. View at: Google Scholar
 T. Irvine, An Introduction to the Shock Response Spectrum, Arizona State University, Tempe, AZ, USA, 2002.
 N. T. Davie and V. I. Bateman, “Pyroshock simulation for satellite components using a tunable resonant fixture—phase 2,” Sandia National Labs, Albuquerque, NM, USA, 1997, Sandia report SAND93 2294. View at: Google Scholar
 T. J. Dwyer and D. S. Moul, “Pyro shock simulation: experience with the MIPS simulator,” in Proceedings of the Space Simulation Conference: Support the Highway to Space Through Testing, pp. 125–138, Williamsburg, VA, USA, 1988. View at: Google Scholar
 Y. J. Mao, H. J. Huang, and Y. X. Yan, “Numerical techniques for predicting pyroshock responses of aerospace structures,” Advanced Materials Research, vol. 108–111, pp. 1043–1048, 2010. View at: Publisher Site  Google Scholar
 A. R. Kolaini and J. P. Fernandez, “Qualifying flight hardware for pyroshock environments: shock simulation systems and modeling,” in Proceedings of the Workshop on Spacecraft Shock Environment and Verification, p. 20, Noordwijk, Netherlands, 2015. View at: Google Scholar
 Y.W. Kim, J.K. Jang, and J.R. Lee, “Pyroshock simulation algorithm in temporal and spectral domains based on laser shock scanning and iterative decomposition and synthesis considering stop band effects,” Shock and Vibration, vol. 2017, Article ID 8351791, 19 pages, 2017. View at: Publisher Site  Google Scholar
 B.H. Jung, Y.W. Kim, J.R. Lee, and D. S. Kim, “Visualization of pyroshock wave reduction by insulator using a laser shock based simulation method,” Measurement, vol. 137, pp. 302–311, 2019. View at: Publisher Site  Google Scholar
 Y. Choi and J.R. Lee, “Multidirectional adjacent wave subtraction and shifted time point mapping algorithms and their application to defect visualization in a space tank liner,” NDT & E International, vol. 86, pp. 53–64, 2017. View at: Publisher Site  Google Scholar
 J. Lee, J.H. Han, Y. Lee, and H. Lee, “A parametric study of ridgecut explosive bolts using hydrocodes,” International Journal of Aeronautical and Space Sciences, vol. 16, no. 1, pp. 50–63, 2015. View at: Publisher Site  Google Scholar
Copyright
Copyright © 2019 YongWoon Kim et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.