Tsiolkovsky rocket equation

Δv from Isp (or ve) and mass ratio.

SIDUS educational calculator. Category propulsion. Tags: delta-v, propulsion. Pure SI. Not flight software.

Formula

Δv = I_sp g₀ ln(m₀ / m_f)

Tsiolkovsky ideal rocket

Primary sources

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.

Open interactive tool · SIDUS