Gravity turn ascent profile optimization with a staged delta-v budget model.
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Updated
Aug 11, 2026 - Python
Gravity turn ascent profile optimization with a staged delta-v budget model.
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.
Core principles and mathematical models for rocketry and orbital mechanics, implemented in code.
Independent orbital mechanics project analyzing Δv sensitivity of plane-change timing in simplified Hohmann-type altitude transfers.
Cited reference tables for space-mission cost and mass estimation: launch vehicles, propellants with derived tankage, delta-v segments, operational costs, and storage systems. EconomicSpace subrepo
Delta-v planner for circular-to-circular transfers (Hohmann, bi-elliptic, plane-change). Impulsive burns, quick trade-offs. Python 3.10+.
Pure Standard ML orbital mechanics: vis-viva, circular/escape velocity, Hohmann and bi-elliptic transfers, Tsiolkovsky rocket equation, sphere of influence (MLton + Poly/ML)
Systems-level quantitative feasibility study of Mars colonization under strict scientific and engineering constraints.
Interactive astrodynamics app for designing interplanetary transfer trajectories using Lambert's problem and real planetary ephemerides.
v2.6 refines 3I/ATLAS analysis with automated peak detection, improved Δv modelling, Ni/Fe compositional anomaly, colour–brightness evolution, and multi-station validation of post-perihelion noise events.
Python-based orbital mission planner for realistic spaceflight and orbital mechanics calculations (KSP-RSS-Principia inspired)
Minimum-Δv impulsive maneuver planning for spacecraft relative orbits - a finite-difference-verified Rust port of the Koenig & D'Amico (IEEE TAC 2020) fuel-optimal impulsive control algorithm.
Interactive Python tool that computes asteroid rendezvous launch windows using Lambert transfers, Earth ephemerides, and user-defined orbital elements.
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