Mission sizing reference
Illustrative array area = power ÷ 250 W/m² net delivered power; this is an explicit sizing assumption, not spacecraft telemetry. GPU figures are vendor maximum TDP, not this workload:
H100 SXM ·
T4.
Run the analysis to see the results.
What these power values include
AKD1500: calibrated chip-power estimate; host processor, memory and supporting circuitry are not included. Jetson: module power (VDD_IN), not GPU-only power. AKD1000: development-board sensor.
These are different measurement boundaries, so they do not establish a whole-system power advantage. Equivalent board comparisons require external DC input measurements on both systems, including idle and processing power. Idle-subtracted power is not available here.
* Selected for the flight design describes the intended hardware role; it does not establish flight qualification.