Abstract
A lightweight and compact structural solution for mechanical shock suppression in spacecraft, such as the holddown and release apparatus of satellites, is a critical and thorny issue. In this work, a ring-shaped structure is introduced to isolate mechanical waves within cylindrical shells. The underlying mechanism is that the ring-shaped structure undergoes different forms of deformation to counteract different modes of incident waves. A subwavelength Mn-Cu alloy ring is designed as a shock wave barrier in a typical spacecraft hold-down and release apparatus structure with multimodal wave excitation. We experimentally reveal that the Mn-Cu alloy ring reduces the peak value of the acceleration frequency response by 53.4% within a wide frequency range from 1 to 10 kHz. Meanwhile, in the time domain, the instantaneous acceleration peak can be weakened by 37.9%. This work provides a new strategy for shock control of shell structures in aerospace engineering and related fields.
| Original language | English |
|---|---|
| Pages (from-to) | 4870-4880 |
| Number of pages | 11 |
| Journal | AIAA Journal |
| Volume | 62 |
| Issue number | 12 |
| DOIs | |
| State | Published - Dec 2024 |
Keywords
- Aerospace Engineering
- Cylindrical Coordinate System
- Cylindrical Shell Structures
- Finite Element Method
- Frequency Response
- Numerical Simulation
- Satellites
- Shock Waves
- Spacecraft Structures
- Spacecrafts
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