Orbital Antares - Manual (Page 93)

Antares
®
OSP-3
User’s Guide
Appendix A
– Payload Questionnaire
Release 1.1 July 2013 A-7
MECHANICAL INTERFACE
DIAMETER Describe Diameter of Interface (e.g. Bolt Circle, Separation System, etc.) and provide illustration
if available:
SURFACE
FLATNESS Flatness Requirements for Sep System or Mating Surface of Launch Vehicle:
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:
FAIRING
ACCESS Payload Fairing Access Doors (spacecraft coordinate frame):
Longitudinal  in  cm Clocking (deg), Describe:
Longitudinal  in  cm Clocking (deg), Describe:
Longitudinal  in  cm Clocking (deg), Describe:
DYNAMICS Spacecraft Natural Frequency:
Axial Hz Lateral Hz
Recommended:
> TBD Hz > TBD Hz
OTHER Other Mechanical Interface Requirements: