--- title: Titan-Hohmann-Transfer-Orbit license: apache-2.0 datasets: - name: Titan-Hohmann-Transfer-Orbit tags: - space - synthetic - mission-simulation - foundation-model - titan size_categories: "700" task_categories: - other --- # **Titan-Hohmann-Transfer-Orbit Dataset Card** **Author:** A Taylor **Contact:** [hf.co/taylor658](https://hf.co/taylor658) **License:** [Apache License 2.0](https://www.apache.org/licenses/LICENSE-2.0) --- ## **Dataset Summary** The **Titan-Hohmann-Transfer-Orbit** dataset simulates an interplanetary mission to Titan using advanced propulsion systems and gravitational assist techniques. This **synthetic dataset** is designed to review: - **Trajectory optimization algorithms** - **Electric propulsion system modeling** - **Mission risk assessment** - **Machine learning training** for aerospace and trajectory decision-support systems. --- ## **Mission Profile** 1. **Earth Departure**: The spaceprobe begins its journey with a launch vehicle, departing Earth’s orbit and entering a heliocentric transfer trajectory. 2. **Gravity Assist Phase**: The spaceprobe utilizes planetary flybys (e.g., Jupiter) to optimize its trajectory toward Saturn and Titan. 3. **Heliocentric Cruise**: The spaceprobe completes extended low-thrust propulsion arcs using Hall Effect thrusters, further refining its trajectory. 4. **Titan Arrival**: Final adjustments are made for spaceprobe orbital insertion to commence Part Two of the mission profile including EDL of floating probes to study Kraken Mare and EDL of a communication relay near Kraken Mare to enable efficient floating probe - earth data transmission. --- ## **Columns (Relevant for Foundation Model Training)** 1. **Initial_Total_Mass** - Total spaceprobe mass (kg) at the mission start, including fuel and payload. 2. **Dry_Mass** - Spaceprobe mass without propellant (kg), useful for estimating burn times and fuel efficiency. 3. **Thrust_Level** - Thrust output of the Hall Effect thrusters (mN). 4. **Launch_Vehicle** - Categorical data specifying the type of launch vehicle used (e.g., “Falcon Heavy,” “SLS”). 5. **Mission_Segment** - Categorical description of the mission phase (e.g., “Launch,” “Cruise,” “Gravity Assist,” “Titan Arrival”). 6. **Time_of_Flight_days** - Elapsed time from mission start, measured in days. 7. **Orbital_Radius_km** - Radial distance from the central celestial body (e.g., Earth, Sun, or Titan). 8. **Semi_Major_Axis_km** - Semi-major axis of the spaceprobe’s elliptical trajectory (km). 9. **Eccentricity** - Describes the shape of the orbit (0 = circle, <1 = ellipse). 10. **Inclination_deg** - Orbital plane tilt relative to the ecliptic or other reference plane. 11. **True_Anomaly_deg** - Position of the spaceprobe along its orbital path. 12. **DeltaV_Used_km_s** - Total accumulated ∆v (km/s) expended since mission start. 13. **Thrust_Events_Start_Time** - Timestamp indicating the start of a thrust event. 14. **Thrust_Events_Stop_Time** - Timestamp indicating the end of a thrust event. 15. **Closest_Approach_Distance_km** - Distance at closest approach during gravity-assist flybys. 16. **Relative_Velocity_km_s** - Velocity of the spaceprobe relative to the flyby planet or Titan upon approach. 17. **Final_Orbit_SMA_km** - Semi-major axis of the final orbit around Titan (km). 18. **Final_Orbit_Inclination_deg** - Inclination of the spaceprobe’s orbit around Titan after insertion. --- ## **Intended Usage** - **Foundation Model Training**: Suitable for time-series and tabular data modeling in the context of interplanetary trajectories. - **Synthetic Orbital Analysis**: For exploring gravity assists, electric propulsion, and mission design principles. --- ## **License & Citation** **License:** [Apache 2.0](https://www.apache.org/licenses/LICENSE-2.0) ```bibtex @dataset{titan_hohmann_transfer_orbit_2024, title={{Titan-Hohmann-Transfer-Orbit Synthetic Dataset}}, author={A Taylor}, howpublished={\url{https://hf.co/taylor658}}, year={2024}, note={Synthetic dataset simulating an interplanetary mission to Titan.} }