Platform

The operating stack for energy-aware spacecraft compute.

EnergyIR turns mission workloads into low-energy onboard execution paths, then reports the energy, quality and proof record behind every result.

Platform architecture

From energy-aware compiler to certified mission output.

EnergyIR is built around measurably lower-energy computation. For spacecraft, that becomes an end-to-end platform: compile the workload, schedule it under mission constraints, run it close to data, and produce evidence.

ThermoIR Compiler

Device-independent compilation to the optimal backend.

ThermOS Runtime

Mission-aware scheduling, energy and fidelity management.

Thermemory

Maximize data residency. Minimize movement.

Ecert Assurance

Cryptographic certificates for every computation.

Developer and mission interface

Prototype like software. Deploy like flight infrastructure.

Ground teams should be able to test workloads through familiar interfaces, compare energy and quality tradeoffs, then freeze an execution path that can survive spacecraft constraints. The EnergyIR platform model gives developers a controllable surface without hiding the physics.

ENERGYIR PLATFORM JOB
mission.load("eo-triage")
  .set_budget(power="tight", latency="real-time")
  .compile(targets=["software", "PB64", "CLAS16"])
  .run(onboard=true)
  .certify() -> result + energy + proof

Interface contract

What the platform returns besides the answer.

Open interface

Expose workloads through familiar API or SDK patterns during ground testing, then freeze the compiled path for the flight target.

Quality budget

Set acceptable fidelity, latency and energy limits so the runtime can choose the lowest-energy route that still satisfies the mission.

Telemetry hooks

Return energy, data movement, timing, backend and caveat metadata alongside the result.

Certificates

Export signed artifacts for post-pass review, procurement evidence or independent verification.

Onboard execution loop

Keep the decision loop inside the spacecraft.

The platform is designed for the mission moment when raw data is abundant, downlink is scarce and waiting for Earth creates operational risk.

01

Sense

Payload, bus or navigation data enters the local compute loop.

02

Classify

EnergyIR decides which work deserves full processing, approximation, deferral or discard.

03

Compute

Runtime maps work to available CPU, GPU, PB64, CLAS16 or resident-memory paths.

04

Certify

Result, backend, fidelity, energy and caveats are recorded as mission evidence.

05

Transmit

Downlink the decision, priority data or certificate instead of raw noise.

Integration model

From candidate workload to mission-ready compute path.

01

Workload intake

Identify the mission loop, target model, data movement, fidelity requirements and operating envelope.

02

Ground characterization

Run representative workloads through software baselines, benchmark harnesses and EnergyIR candidate paths.

03

Backend selection

Select CPU, GPU, PB64, CLAS16 or hybrid execution depending on energy, latency and verification requirements.

04

Flight packaging

Package runtime controls, telemetry hooks, fallbacks and proof artifacts for mission software.

05

Assurance review

Document measured results, projections, caveats, repeatability and verification path before operational use.

Benchmark and proof layer

Measured, modelled and projected stay separate.

Every result says which hardware path ran, what was measured, what was projected, what caveats apply and which certificate can be checked later. Measured savings and proof are the discipline the platform is built on, and the spacecraft stack keeps it explicit.

Mission fit

Request the platform architecture brief.

The brief is the right next step for technical teams evaluating compiler interfaces, onboard runtime constraints, hardware fit or certificate requirements.

Trust signals

Built for mission environmentsDesigned for radiation-aware computeBenchmark-backed architectureExport-control aware collaboration