Low Fidelity Space Systems Analysis Tools-Heliocentric Trajectory Tool(LAR-18744-1)

This tool is produced is take advantage of pre-existing resources of known lambert trajectory solutions to various bodies, NEA's and more. This database is created and maintained by Ames Research Center and provides a two significant figure estimate of the injection deltaV to get to the desired orbit and the insertion dV to stop at the location. Additionally, it does calculate flyby maneuver effects.