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Antares, Osp-3 user’s guide, Appendix a – payload questionnaire – Orbital Antares User Manual

Page 94

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Antares

®

OSP-3

User’s Guide

Appendix A

– Payload Questionnaire

Release 1.1

July 2013

A-8

ELECTRICAL INTERFACE

Bonding Requirements:

Are Launch Vehicle Supplied Pyro Commands Required?

Yes / No If Yes, magnitude: amps for msec

When ________ seconds before separation

Are Launch Vehicle Supplied Discrete Commands Required?

Yes / No

If Yes, describe:

Is Electrical Access to the Satellite Required?

After Encapsulation?

Yes / No

At Launch Site?

Yes / No

Is Spacecraft Battery Charging Required?

After Encapsulation?

Yes / No

At Launch Site?

Yes / No

Is a Telemetry Interface with the Launch Vehicle Flight Computer Required?

Yes / No


If Yes, describe:


Other Electrical Requirements (e.g.; coax, fiber, etc.):



Please complete attached sheet of required pass-through signals.

RF RADIATION

Time After Separation Until RF Devices Are Activated:

(Note: Typically, spacecraft radiation is not allowed from encapsulation until after fairing separation.)


Frequency: MHz

Power: Watts

Location(s) on Spacecraft (spacecraft coordinate frame):

Longitudinal  in  cm

Clocking (deg), Describe:


Longitudinal  in  cm

Clocking (deg), Describe: