Avionics Suite
AssemblyTriple-redundant flight computers that fly ascent and then, with no one in the loop, fly the booster’s entry and landing; an autonomous flight-termination system replaces the traditional ground-commanded destruct. A full specification article for this item is being written. Meanwhile its bill of materials and connections are below.
Bill of materials for Avionics Suite
10 top-level lines as of r141143| # | Item / sub-assembly | Part no. | Qty/assy | Ext. qty | Parts | Type |
|---|---|---|---|---|---|---|
| 1 | Flight Computer 4 parts | orbital-launch-vehicle-flight-computer | 3× | 3 | 0 | assembly |
| 2 | Inertial Measurement Unit | orbital-launch-vehicle-imu | 3× | 3 | · | part |
| 3 | GPS Receiver | reusable-launch-vehicle-gps-receiver | 3× | 3 | · | part |
| 4 | Radar Altimeter | reusable-launch-vehicle-radar-altimeter | 2× | 2 | · | part |
| 5 | Telemetry Transmitter | orbital-launch-vehicle-telemetry-transmitter | 2× | 2 | · | part |
| 6 | Autonomous Flight Termination Unit | reusable-launch-vehicle-afts-unit | 2× | 2 | · | part |
| 7 | Vehicle Battery 2 parts | orbital-launch-vehicle-battery | 4× | 4 | 0 | assembly |
| 8 | Power Distribution Unit 6 parts | reusable-launch-vehicle-power-distribution-unit | 2× | 2 | 0 | assembly |
| 9 | Flight Data Network 3 parts | reusable-launch-vehicle-data-network | 1× | 1 | 0 | assembly |
| 10 | Sensor Junction Box 5 parts | reusable-launch-vehicle-sensor-junction-box | 6× | 6 | 0 | assembly |