Execute deployment cycle of the active thermal radiator subsystem, verify heat rejection exceeding 40 kW under steady state, and retract to stowed configuration.
In vacuum, spacecraft cannot shed waste heat by convection. Without active radiative cooling, avionics and reactor heat steady-state power loads drive the hull toward thermal limits. Deploying the external radiator wings increases radiative surface area and rejects heat into deep space via Stefan-Boltzmann emission.
The spacecraft begins with radiator panels stowed and internal temperature elevated above 365 K:
[THERM_RAD] frames for panel deployment state and core temperature in Kelvin.{"radiator_cmd": {"state": "DEPLOYED"}} and wait for the deployment transit to complete.Ask Antigravity to inspect the thermal radiator specification and complete mission T0-03:
Read the Thermal Radiator specifications at /api/specs/hardware/radiator.
Update our flight computer to complete mission T0-03:
1. Command the radiator wings to DEPLOYED.
2. Maintain attitude rates below 0.50 deg/s while monitoring [THERM_RAD] telemetry until core temperature cools below 340.0 K for 3.0 seconds./api/specs/hardware/radiator to review deployment transit timing, radiative cooling capacity, and structural rate limits.