Taylor658/titan-hohmann-transfer-orbit

🪐 Titan-Hohmann-Transfer-Orbit Dataset

🛰️ A 700-row synthetic dataset simulating an interplanetary mission to Titan using Hall Effect electric propulsion and gravity assists, from Earth departure through Titan orbital insertion.

⚠️ Disclaimer: All values are synthetically generated from simplified orbital mechanics models. This is not flight data and is not suitable for mission planning.

📋 At a Glance

📝 Dataset Summary

The Titan-Hohmann-Transfer-Orbit dataset simulates an interplanetary mission to Titan using electric propulsion and gravity assist techniques. It is designed for:

• —🧭 Trajectory optimization algorithm development
• —⚡ Electric propulsion system modeling
• —🎲 Mission risk assessment exercises
• —🤖 Model training and evaluation for aerospace and trajectory decision-support systems

🛸 Mission Profile

1. 1.🌍 Earth Departure: The spaceprobe departs Earth orbit on a launch vehicle and enters a heliocentric transfer trajectory.
2. 2.🪐 Gravity Assist Phase: Planetary flybys (e.g., Jupiter) shape the trajectory toward Saturn and Titan.
3. 3.☀️ Heliocentric Cruise: Extended low-thrust arcs using Hall Effect thrusters refine the trajectory.
4. 4.🛰️ Titan Arrival: Orbital insertion, followed by Part Two of the mission profile: Entry, Descent, and Landing (EDL) of floating probes to study Kraken Mare, Titan's largest methane sea, and EDL of a communication relay near Kraken Mare to link the probes with Earth.

🏗️ Dataset Structure

💡 Usage

🚀 Load the Dataset

from datasets import load_dataset

dataset = load_dataset("Taylor658/titan-hohmann-transfer-orbit", split="train")
print(dataset[0])

🎯 Intended Usage

• —📈 Time series and tabular modeling of interplanetary trajectories
• —🧭 Synthetic orbital analysis: gravity assists, electric propulsion, and mission design principles
• —🧪 Benchmarking trajectory prediction against closed-form Hohmann and patched-conic solutions
• —🔗 Companion resources: the Titan-Hohmann fine-tuned model and the HohmannHET physics library

⚠️ Limitations

🧬 Synthetic Content

• —All rows are generated from simplified orbital mechanics and propulsion models
• —Values do not correspond to any flown or planned mission

📏 Physics Simplifications

• —Two-body and patched-conic assumptions; no full n-body integration
• —Thruster performance is idealized; no degradation or power-limiting effects

📦 Scale

• —700 rows is sufficient for prototyping and evaluation, not for training large models from scratch

🚫 Not for Mission Planning

• —Outputs must be validated against a flight-qualified astrodynamics toolchain before any operational use

🙌 Citation

@dataset{titan_hohmann_transfer_orbit_2026,
  title={{Titan-Hohmann-Transfer-Orbit Synthetic Dataset}},
  author={Taylor, A.},
  howpublished={\url{https://huggingface.co/datasets/Taylor658/titan-hohmann-transfer-orbit}},
  year={2026},
  note={Synthetic dataset simulating an interplanetary mission to Titan.}
}

🧑‍💻 Contributing

• —💬 Open a Discussion to request additional mission segments, propulsion models, or target bodies

👨‍🚀 Author: A Taylor · 🤗 Hugging Face: hf.co/Taylor658 · 🐙 GitHub: ATaylorAerospace