Orbital Minotaur VI - Manual (Page 50)

Minotaur IV • V • VI User’s Guide Section 4.0 – Payload Environment
events and load cases. Results from the CLA are reported in the Acceleration Transformation Matrix
(ATM) and Load Transformation Matrix (LTM) as requested by the payload provider. A payload isolation
system is available as a non-standard option and is described in Section 8.10. This system has been
demonstrated to significantly reduce transient dynamic loads that occur during flight.
Figure 4.1.1-1. Payload CG Net Transient Lateral Acceleration (Minotaur IV)
Figure 4.1.1-2. Payload CG Net Transient Lateral Acceleration (Minotaur IV+, V, VI, and VI+)
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