Compare launch windows and flight times for your mission.
Sun-centered Lambert preview at the selected dates. Metrics use the precomputed grid. *Δv = departure + arrival v∞; excludes spacecraft burns.
Open mission plannerA web-based platform for early-stage space mission design. LOTUS brings trajectory synthesis, spacecraft sizing, trade-space exploration, and systems engineering review into one workspace, instead of stitching those together across separate tools.
