User Manual

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: