AERO-OPS

Mission Operations Platform v0.3.0

Cloud-Native Microservices • SQLite WAL • JSON-RPC 2.0 MCP • Multi-Propellant CFD • AST Sandbox

CONNECTING GATEWAY...
MCP JSON-RPC 2.0 (7 TOOLS)
AST SANDBOX v2
🚀 3-DoF Flight Dynamics
Apogee Altitude
14,285 m
Peak Velocity
Mach 2.45
Max-Q Pressure
58.4 kPa
Recovery Landing
5.8 m/s
🛰️ SGP4 Orbital Tracker
Altitude
418.5 km
Velocity
7.66 km/s
Next AOS
06:14:22 UTC
Max Elevation
68.4°
🌪️ Transonic CFD Surrogate
Airfoil
NACA 2412
Angle of Attack
α = 4.0°
Lift Coeff (CL)
0.6842
Drag Coeff (CD)
0.00941
🏆 SWE-bench / Handshake AI Leaderboard
Model Name Domain / Scope Resolution Evals Status
Human Expert Baseline Propulsion / Flight ODEs 100.0% 8/8 VERIFIED
Claude 3.5 Sonnet Compressible Gas Dynamics 87.5% 7/8 RESOLVED
GPT-4o Astrodynamics & Orbits 62.5% 5/8 RESOLVED
DeepSeek-Coder V2 Vortex Panel CFD Solvers 62.5% 5/8 RESOLVED
Qwen-2.5-Coder 32B Aerospace Numerical ODEs 50.0% 4/8 RESOLVED
⚡ MCP (Model Context Protocol) JSON-RPC Portal
[MCP] Ready. Select tool and click "Invoke MCP Tool" to execute JSON-RPC 2.0 simulation tool.
🤖 Handshake AI Sandboxed Code Evaluation Workbench
Select a task to inspect problem statement and fail-to-pass specifications.
[BENCHMARK] Try "Load Buggy Starter" vs "Load Gold Solution" and click "Run Patch Evaluation" to verify real fail-to-pass behavior.
🗄️ SQLite ACID Telemetry & Evaluation Database Audit Trail
Run ID / UUID Mission Name Status Apogee (km) Max Mach Max-Q (kPa) Duration (s) Timestamp (UTC)
Loading database records...
🌌 Unified Multi-Disciplinary Aerospace Mission Orchestrator
Phase 1: Propulsion
c* 1685.7 m/s
A/A* = 8.3 • Δv = 3202 m/s
Phase 2: Trajectory
Apogee 798.5 km
Mach 13.98 • 6 Staging Events
Phase 3: Aerodynamics
L/D = 64.55
NACA 23012 • xcp/c = 0.2817
Phase 4: Orbital Transfer
Δv = 115.7 m/s
200km → 400km ISS (45.3 min)
[STATUS] Ready. Click "Run End-to-End Mission" to execute real-time multi-stage simulation across all 4 aerospace physics engines.
🔥 Supersonic Rocket Nozzle CFD & Shock Diamond Lab (nozzle-cfd-propulsion)
Nozzle Exit Mach
3.44
Specific Impulse Isp (Vac)
295.1 s (325 s)
Peak Bartz Throat Flux
55.5 MW/m²
Flow & Plume Regime
OVEREXPANDED SHOCKS