User Manual

Antares
®
OSP-3 User’s Guide Section 4.0 – Payload Environments
Release 1.1 July 2013 28
4.3. Payload Shock Environment
The maximum shock response spectrum at the base of the payload from all launch vehicle events will not
exceed the flight limit levels provided in Figure 4.3-1. The flight limit levels are derived from ground sepa-
ration test data and analytical predictions for the vehicle and payload separation systems. These levels
are applicable to a payload using the Antares optional payload separation system or attaching to the non-
separating interface.
Figure 4.3-1. Antares Payload Maximum Flight Level Shock at the Base of the Payload