User Manual

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: