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Supports multi-body topology with rotational/translational joints and rigid/flexible bodies, enabling accurate simulation of complex spacecraft structures as detailed in the README.

Models two-body and three-body orbits from low Earth orbit to deep space, allowing for diverse mission scenarios across the solar system.

Enables concurrent simulation of multiple spacecraft for studies like rendezvous and formation flying, facilitating complex mission analysis.

Balances fast setup for concept studies with rigorous features for full spacecraft development, supporting the entire lifecycle from design to test.