Orbital Minotaur VI - Manual (Page 28)

Minotaur IV • V • VI User’s Guide Section 2.0 – Minotaur IV Configurations
2.3.6.3. Minotaur VI
The Minotaur VI launch vehicle, shown in Figure
2.3.6.3-1, provides 1800-3200 kg (4000-7000 lbm)
to Low Earth Orbit (LEO). Minotaur VI is a natural,
low-risk evolution to the successful Minotaur IV
vehicle family, adding an additional Peacekeeper
Stage 1 (SR118) below the existing Minotaur IV+
stack (SR118-SR119-SR120-STAR 48BV). The
new design elements of Minotaur VI are based on
existing components, thereby minimizing risk.
Minotaur VI leverages heavily off the successful
Minotaur IV+ vehicle, using the same front section
assembly. All avionics, ordnance, and pneumatics
components are already qualified for Minotaur VI
environments. All mechanical structures have been
designed and qualified to loads that encompass
Minotaur VI with the exception of the payload
interface
cone. However, payload cone
qualification is deemed low risk due to the safety
margins predicted for Minotaur VI loads. Minotaur
VI does not require new support equipment and
only requires minor procedural changes to use
existing Minotaur IV equipment and processes for
integration and test activities.
Existing facilities and infrastructure at Kodiak
Launch Complex (KLC) and Launch Complex 46
(LC-46) at CCAFS can accommodate Minotaur VI.
The Minotaur VI launch system complies with
range safety requirements RCC-319 and EWR
127-1, as tailored for Minotaur IV.
Figure 2.3.6.3-1. Minotaur VI Vehicle
Configuration
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