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Orbital Antares User Manual

Page 93

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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: