Orbital Antares User Manual
Page 37

Antares
®
OSP-3
User’s Guide
Section 4.0
– Payload Environments
Release 1.1
July 2013
26
4.2. Payload Vibration Environment
The random vibration environment at the payload interface is encompassed by acoustics and coupled
loads analysis results. Antares does not have a specific random vibration environment for the payload.
4.2.1. Payload Acoustic Environment
The maximum expected acoustic levels within the Antares fairing are shown in Figure 4.2-1. Antares
peak acoustic environments occur at lift-off and near the point of maximum dynamic pressure. Acoustic
levels are sensitive to spacecraft geometry (fill factor), so payload specific adjustments may be neces-
sary.
Figure 4.2-1. Antares Fairing Internal Maximum Flight Level Payload Acoustic Environment
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- GQM-163A Coyote (2 pages)
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- Minotaur I (2 pages)
- Minotaur VI (2 pages)
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- Minotaur IV (2 pages)
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- AIM (2 pages)
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