AVS Public Document

Text from public EtherPad.

Estimates
Volume includes LIDAR, 30 sensors of 10cm x 10cm x 10cm, and control panels of 3m^2 x 30cm deep. Assumes wiring will be primarily routed within control panels. Conduit running throughout cabin is of minimal additional volume.
 * Mass: 700-800 kg
 * Power: 350-400 W
 * Volume: 2.76 m^3

Thermal Info Required/Collaboration between groups
From Propulsion group: You may have to find a way to coordinate which RCS rockets fire on which module when the modules are attached together. You'll probably need a lot more detailed infor about the thrusters that we wont have until after PDR
 * Avionics temperature requirements
 * Confirm that the Avionics group will be in charge of cooling their equipment, and then Thermal will just need to consider how much heat is generated.
 * Method(s) of cooling avionics. Air-cooled (therefore adding heat to the crew cabin air), liquid cooled (where the liquid can pump heat more directly to the radiators), or some other method?