Ceres to Pallas Transfer
Main belt asteroid transfer between two large bodies
This is demonstration data showing the capabilities of ADAM's transfer trajectory service.
Porkchop Plot
Transfer Details
Download Raw Data
File Format Information: All data files were generated using the adam_core library.
Transfer data is provided in CSV format containing all computed Lambert transfer solutions with trajectory details, orbital elements, and launch directions. The accompanying CSV-W metadata file contains detailed schema information including column descriptions, units, coordinate frames, and byte-level indexing for efficient data access.
For data analysis, we recommend the parquet format, which provides the most efficient access to the complete dataset with built-in schema information and is optimized for high-performance analysis with adam_core, pyarrow, pandas, dask, or spark.
Ephemeris files are provided in OEM format (Orbit Ephemeris Message), a CCSDS standard.
CSV file with all computed transfer trajectories and ra/dec
Schema and indexing metadata for the CSV file
Recommended: Parquet format with optimized schema for efficient data analysis to be used with adam_core.
Standalone HTML file with porkchop plot
OEM file with departure body orbital data
OEM file with arrival body orbital data
Explore Data with adam_core
Python Analysis: You can load and analyze the trajectory optimization data directly in Python using the adam_core library. The code below shows how to access C3 values, V-infinity, time of flight, and orbital elements.
About This Demo
This demonstration showcases ADAM's Trajectory Optimizer service using real computational results from an Earth-Mars transfer analysis. The service uses Lambert's problem solver to compute optimal transfer trajectories between solar system bodies.
To run your own trajectory analysis with custom parameters,create an account..