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    What are mass and volume of your platform?

    What is the maximum mass/volume available for the propulsion system? Please, consider also tanks and propellant.

    How much electrical power is available for propulsion system? Please, indicate max and average power available and for how long if possible.

    What kind of maneuver can you allow for an IOD (e.g., orbit change, attitude variation)?

    In case of orbit change, how much is the delta-altitude that your platform can sustain/compensate?

    How much is the the maximum rotation angle, maximum torque and angular momentum that your platform can sustain/compensate?

    Which are the available electrical interfaces for power (e.g., connectors, voltage, max current, regulated or not)?

    Which are the available electrical interfaces for communication?

    How are communications with the PS handled e.g., (through the satellite, directly) and what protocols are available?

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