Circularize burn
Δv to circularize an ellipse at periapsis or apoapsis.
SIDUS educational calculator. Category orbital. Tags: delta-v, GNC, maneuver, orbital. Pure SI. Not flight software.
Formula
Δv = |v_ell − v_c| at apsis
Circularize an elliptical orbit
Primary sources
- Fundamentals of Astrodynamics and Applications (David A. Vallado): Standard reference for two-body, Lambert, maneuvers, and J2. Equations implemented independently in SIDUS.
- Orbital Mechanics for Engineering Students (Howard D. Curtis): Textbook derivations for Hohmann, vis-viva, rocket equation, elements.
- Spaceflight Dynamics (William E. Wiesel): Relative motion, rendezvous, and phasing context complementary to Vallado/Curtis.
How do AI agents use this tool?
Read /llms.txt or call https://sidus.tools/api/mcp. Open the interactive page for live SI inputs.