Calculate Optimal Design of Rocket Propulsion Systems (Kerbal Space Program).
Advanced rocket trajectory simulation and design optimization system with parallel optimization algorithms and supersonic flight regime detection. Optimizes diameter, nose cone length, and body length to achieve target apogee within tolerance.
A paper-design tool for KSP RSS/RO/RP-1 launch vehicles — auto-generate rocket designs from requirements, pick engines by family with fuzzy search, real-time TWR/Δv verification, and an interactive solar-system Δv map.
Design files for my Tripoli L2 certification rocket.
Four-in-one Windows operations suite for KSP RSS/RO/RP-1: program planning, save-linked rocket design, launch control, and mission telemetry.
ENMA: Empirical Nozzle optimization & Mach distribution Analysis for liquid propellant rocket engines.
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