Interactive · No external APIs
Mission Chip Configurator
Run onboard inference when downlink is limited, radiation is hostile, and power is measured in watts. Tune the mission — OrbitChip maps orbit class, duration, payload, and autonomy into a recommended die profile, fit score, and risk matrix locally.
Mission constraints
Select the orbit you are actually flying — the engine maps radiation, power, and thermal stress locally.
Orbit class
Recommended silicon
OC-X1 LEO Radiation-Aware Inference Module
X1 — LEO / rideshare class
Mission fit
95
Radiation readiness
High
Model index / qualification envelope
Power envelope
18W
Steady-state inference estimate
Ceiling 24W
Headroom 6W
Thermal margin
25%
Power headroom vs declared bus ceiling
Thermal risk: Low
Risk matrix
- low
Total ionizing dose (TID) margin
Readiness High (86/100 model index).
- medium
Single-event upset (SEU) exposure
LEO trajectory class.
- low
Thermal coupling / dissipation
Moderate — nominal spacecraft bus — 25% power headroom.
- low
Inference duty cycle vs downlink
Supervised autonomy — workload Detect & track — streaming vision.
Inference TOPS
66
Latency (est.)
36 ms
Redundancy
Single module acceptable with periodic ground check.
Mission spec sheet
ORBITCHIP · CONFIDENTIAL| Orbit class | LEO — low Earth orbit |
| Mission duration | 6 months — 2 years |
| Payload | Earth observation |
| Sensor path | Optical / multispectral |
| Power budget (bus) | 12 — 24 W |
| Estimated compute draw | 18W |
| Power headroom | 6W |
| Radiation readiness | High |
| Radiation index | 86/100 |
| Thermal risk | Low |
| Thermal margin index | 25% headroom |
| Inference throughput | 66TOPS (INT8-equiv.) |
| Inference latency | 36ms (median est.) |
| Recommended silicon | OC-X1 LEO Radiation-Aware Inference Module |
| Chip class | X1 — LEO / rideshare class |
| Redundancy | Single module acceptable with periodic ground check. |
| Mission fit | 95/100 |
| Engine revision | orbitchip-engine-2.0.0 |