PPolySim OS
Use case · powered by Pitot-Tube Airspeed

Pitot-Tube Airspeed for a rocket ascent

Simulate a rocket ascent live in your browser. This runs the real Pitot-Tube Airspeed solver — adjust the inputs, watch it respond instantly, and export the result. No install, no account.

Pitot-Tube AirspeedLive

Controls

Presets

A pitot tube measures the pressure difference between still and moving air, then airspeed follows from v = √(2Δp/ρ). Because air thins with altitude, true airspeed exceeds the indicated value up high — a key gotcha in aviation. Educational tool.

▶ Run in Python

Data Inspector

Air density1.225 kg/m³
True airspeed49.5 m/s
Indicated airspeed49.5 m/s
Mach number0.145

Governing equation

Reading this result: Near sea level the air is close to standard density, so true airspeed and indicated airspeed nearly coincide — the gauge reads reality directly.

Runs locally in your browser — free forever. Scale to the cloud when reality gets heavy.

or unlock everything with Pro →

About this simulation

The full Pitot-Tube Airspeed tool models a rocket ascent with the same numerics engineers and scientists use — running entirely client-side. Change any parameter and the result updates in real time, so you can build intuition, check a design, or teach the concept without spreadsheets or installs.

More you can do with Pitot-Tube Airspeed

Other ways to simulate a rocket ascent

Frequently asked questions

How do I simulate a rocket ascent?
Open this page and use the live Pitot-Tube Airspeed tool below — set your inputs and the simulation runs instantly in your browser using real numerics. No install, no account needed.
Is it free?
Yes. The simulation runs free in your browser. A one-time unlock or a Pro plan adds advanced parameters, saved presets, data import, and clean exports.
Can I use my own numbers?
Absolutely — every input is adjustable, and with data import you can drive a rocket ascent from your own measurements.