Orbital Minotaur VI - Manual (Page 94)

Minotaur IV • V • VI User’s Guide Section 7.0 – Ground and Launch Operations
7.3.2. Final Vehicle Integration and Test
After successful completion of payload mate and fairing closeout, the encapsulated payload is
transported to the pad in a vertical configuration and then lifted atop the booster assembly (see Figure
7.3.1-1). Final post-mate checks of the booster assembly and front section assembly interface are
conducted, followed by a final systems verification test. At this point the vehicle is ready for final Range
interface tests.
7.3.3. Launch Vehicle Arming
Following final vehicle testing, the launch vehicle is armed and the pad is cleared for launch. The majority
of these arming activities occur at L-1 day and bring the Minotaur launch vehicle nearly to its launch day
configuration. L-1 day is also typically the last opportunity for payload access. The last remaining arming
steps (final arming) occur mid-way during the countdown on launch day.
Figure 7.3.1-1. Minotaur Uses Vertical Integration for Each Booster Stage, the Guidance Control
Assembly, and the Encapsulated Payload Assembly
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