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Low Fidelity Space Systems Analysis Tools-Heliocentric Trajectory Tool

A NASA software catalog entry available for reuse or request.

About this technology

Overview

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.