Orbital Minotaur I - Manual (Page 97)

Minotaur I User’s Guide Appendix A
MECHANICAL INTERFACE
DIAMETER Describe Diameter of Interface (e.g. Bolt Circle, etc):
SEPARATION
SYSTEM
Will Launch Vehicle Supply the Separation System? Yes / No
If Yes approximate location of electrical connectors:
special thermal finishes (tape, paint, MLI) needed:
If No, provide a brief description of the proposed system:
SURFACE
FLATNESS
Flatness Requirements for Sep System or Mating Surface of Launch Vehicle:
FAIRING
ACCESS
Payload Fairing Access Doors (spacecraft coordinate frame):
Longitudinal  in  cm Clocking (deg), Describe:
Longitudinal  in  cm Clocking (deg), Describe:
Note: Standard Service is one door
DYNAMICS Spacecraft Natural Frequency:
Axial Hz Lateral Hz
Recommended:
> 35 Hz > 12 Hz
OTHER Other Mechanical Interface Requirements:
Release 3.0 March 2014 A-11