Attach_4_SHOCK_VIBRATION_ShockWave_Isolator_0816_(MOOG).pdf
PDF 881 KB Posted
- Attached to
- Small Rocket Program-Orbital (SRP-O) Agile Small Launch Operational Normalizer-45 (ASLON-45) Federal contract opportunity
- Solicitation number
- FA8818-18-R-0011
About this file
Attachment 4 Shock Vibration ShockWave Isolator (MOOG)
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Attach_3_SMC_Guide_SMC-G-1204_Space_Launch_Readiness_Review_Process-31Oct2013.pdf | ||
| Attach_2_ASLON-45_Combined_Synopsis_Solicitation_QA_for_FBO_Release_(15May19).pdf | ||
| Attach_1_ASLON-45_Combined_Synopsis_Solicitation_(15May19).pdf | ||
| ASLON-45_Final_Combined_Synopsis-Solicitation_Rev_1_(2May19).pdf | ||
| Attachment_1_-_ASLON-45_Combined_Synopsis_Solicitation.pdf | ||
| Attachment_2_-_Combined_RFI_Responses_ASLON-45_14_Dec_18.xlsx | XLSX spreadsheet |
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Text version
Moog’s patent pending ShockWave isolator product family is the perfect solution for small payload and CubeSat launch isolation.
ShockWave leverages over two decades of spaceflight hardware heritage and packages launch worthy technology into a reliable, predictable system at a price point that is comparable to non-aerospace worthy, elastomeric isolation mounts.
KEY FEATURES
• Low-mass, low-profile isolation mounts
• Suitable for shock and random vibration load attenuation
• Configurable with metric and standard interfaces
• Predictable attenuation through an all metallic load path
• Robust performance over the launch operational environment
• Provides greater than 20% of critical damping
PROVIDES VIBRATION ISOLATION FOR THE APPLICATIONS
• CubeSat Dispensers
• Optical Mounts
• Machine Tools
• Electronics Components
• Directed Energy Systems
SHOCK AND VIBRATION I SHOCKWAVE
SHOCKWAVE ISOLATOR
The following table provides measured stiffness values for the
ShockWave part number SW-150-1000-190 across a broad frequency range.
SHOCKWAVE ISOLATOR
©2018 Moog, Inc. All rights reserved.
Product and company names listed are trademarks or trade names of their respective companies. Form 500-1094 0818 linkedin.com/ company/moog-sdg facebook.com/ MoogSDG.USA twitter.com/ MoogSDG
John Howat, Business Development Manager – Moog SAIS West Tel +1 650 417 4285 jhowat@moog.com
Equipment described herein falls under the jurisdiction of the EAR and may require US Government Authorization for export purposes. Diversion contrary to US law is prohibited.
NOMINAL STIFFNESS (SW-150-1000-190)
Description 20 Hz 50 Hz 100 Hz
Axial (lbf/in) 2,300 2,700 3,200
Lateral (lbf/in) 4,400 5,800 7,900
ShockWave was designed with the CubeSat community in mind. The ShockWave isolator is modular and configurable. It will accommodate a wide variety of spacecraft configurations.
The following tables provide predicted frequencies for 3U, 6U, and 12U spacecraft with varying mass. These tables are a guide for specifying quantity and configuration of ShockWave.
3U 4kg, 4 Isolators 6 kg, 6 Isolators 8 kg, 6 Isolators
Mode No. Frequency (Hz) Mode No. Frequency (Hz) Mode No. Frequency (Hz)
1 53 1 53 1 46
2 64 2 67 2 58
3 96 3 96 3 84
6U 8kg, 6 Isolators 12 kg, 8 Isolators 16 kg, 8 Isolators
Mode No. Frequency (Hz) Mode No. Frequency (Hz) Mode No. Frequency (Hz)
1 58 1 55 1 48
2 73 2 68 2 59
3 84 3 80 3 69
12U 16kg, 12 Isolators 24 kg, 12 Isolators 32 kg, 12 Isolators
Mode No. Frequency (Hz) Mode No. Frequency (Hz) Mode No. Frequency (Hz)
1 41 1 34 1 29
2 54 2 44 2 38
3 84 3 69 3 60
MECHANICAL DIMENSIONS (IN INCHES)
VIEW ICD FOR FURTHER DETAIL – METRIC INTERFACE UPON REQUEST
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