Orbital Antares - Manual (Page 94)

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: