User Manual

Antares
®
OSP-3 User’s Guide Section 4.0 – Payload Environments
Release 1.1 July 2013 27
4.2.2. Sine Vibration
Figure 4.2.2-1 defines the maximum flight level payload interface sinusoidal vibration levels for a fixed
base payload test, which may be used for preliminary design. The spectrum defined in this figure is pro-
vided for reference only. Orbital develops a mission-specific sine spectrum for each mission using the
results from CLA.
Figure 4.2.2-1. Antares Payload Interface Sine Vibration Levels