Space Edge Simulation System

The CI/CD Pipeline for Orbital Software.

Test your code against radiation-induced bit-flips, dynamic orbit latencies, and satellite blackouts before you launch. Build resilient space-edge applications with Rust, WASM, and C++.

The Harsh Reality of Space Edge Computing

Standard terrestrial DevOps procedures crash and burn in orbit. Space applications operate under extreme physical environments that must be modeled deterministically.

Cosmic Radiation & Bit-Flips

Ionizing particles and heavy ions strike microprocessors, causing Single Event Upsets (SEU) that flip bits in RAM and registers. Unmitigated, this triggers fatal crashes and instruction memory corruptions.

SEU Simulated Fault Injection

Orbital Network Outages

Leo constellations move at 7.8 km/s, producing extreme Doppler frequency shifts, highly variable round-trip latencies, and regular signal occultation. TCP/IP flows fail completely without specialized network handlers.

LEO/MEO Doppler & Outage Modeling

Unrecoverable Cost of Failure

You cannot ssh into a bricked satellite orbiting 500 kilometers above Earth. A single segmentation fault or deadlock can permanently compromise a cubesat, vaporizing millions of dollars in mission hardware and payload space.

Fatal Bricking Prevention

Hardened for the Space Frontier

SpaceOps equips aerospace software teams with a deterministic simulation ecosystem integrated directly into standard terrestrial GitLab, GitHub, or custom runners.

1. Radiation Fault Injection

Dynamically introduce single-bit flips, double-bit corruptions, and register states errors in RAM arrays during compile testing. Track application fault mitigation, self-correction algorithms (EDAC), and recovery paths.

radiation_test.rs
#[test]
fn inject_cosmic_ray() {
  // Simulates 150 MeV particle impact
  spaceops::inject_fault(MemoryBlock::RAM, 0x0F4A);
  assert_eq!(system.status(), RecoveryMode::Mitigated);
}

2. Dynamic Orbit Networking

Emulate real-world LEO, MEO, or GEO constellation networks. Replicate high Doppler effects, progressive packet drop ratios, and complete satellite line-of-sight occultation based on accurate Keplerian orbital models.

ORBIT NETWORK TEL ACTIVE
Satellite Altitude: 524.3 km
Dynamic RTT: 124ms → 452ms
Symmetrical Drop: 4.21% (Doppler Emulated)

3. WASM & Container Sandbox

Run WebAssembly (WASM), C++, or Rust apps in highly sandboxed, hardware-throttled containers. Mimic exact cubesat flight processor limitations, restricting RAM to 64MB and capping core allocation safely.

spaceops.yaml
sandbox:
  runtime: wasmtime-orbital
  resources:
    memory: 64MB # Max flight hardware RAM
    cpu_cycles: 120MHz # Power saving throttling

Secure Your Orbital Pipeline

Ensure flight software survivability. Apply for our exclusive private beta program and get prioritized waitlist access.