Dynamic pressure (max-q)

ISA density/temp + q = ½ρv² and Mach: launch ascent / aero loads.

SIDUS educational calculator. Category utilities. Tags: aero, launch, operations, structures, utilities. Pure SI. Not flight software.

Formula

q = ½ ρ v² · M = v / a (ISA)

Max-q & Mach on ascent

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