Orbital Minotaur I - Manual (Page 95)

Minotaur I User’s Guide Appendix A
ELECTRICAL INTERFACE
Bonding Requirements:
Are Launch Vehicle Supplied
Pyro Commands Required?
Yes / No If Yes, magnitude: amps for msec
(Standard Service is 10 amps for 100 msec)
Are Launch Vehicles Supplied? Yes / No If Yes, describe:
Discrete Commands Required? Yes / No
Is Electrical Access to the Satellite Required... After Encapsulation? Yes / No
at Launch Site Yes / No
Is Satellite 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:
Please complete attached sheet of required pass-through signals.
RF RADIATION
Time After Separation Until RF Devices Are Activated:
(Note: Typically, no spacecraft radiation is allowed from encapsulation until 30 minutes after liftoff.)
Frequency: MHz
Power: Watts
Location(s) on Satellite (spacecraft coordinate frame):
Longitudinal  in  cm Clocking (deg), Describe:
Longitudinal  in  cm Clocking (deg), Describe:
Release 3.0 March 2014 A-9