For Educators · Rocket Equation
Rocket Equation for a supersonic jet
Built for educators teaching it to a class. Drop a live demo into a lecture or assign it as a shareable link — no lab installs. Simulate a supersonic jet live below — adjust the inputs and watch it respond, right in your browser.
Rocket Equation (Tsiolkovsky)Live
the tyranny of the rocket equation
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Δv = Isp·g·ln(m₀/mf). Because Δv grows only with the log of the mass ratio, reaching orbit (~9.4 km/s) demands enormous propellant fractions — which is exactly why rockets stage.
Data Inspector
Exhaust velocity2.94 km/s
Δv per stage4.74 km/s
Total Δv4.74 km/s
Reaches LEO?no
Governing equation
Reading this result: Short of orbit by 4.7 km/s. Because Δv scales only with ln(mass ratio), raise Isp, lift the mass ratio, or add a stage rather than just adding propellant.
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- Is this good for educators?
- Yes — this version of "Rocket Equation for a supersonic jet" is framed for educators teaching it to a class. Drop a live demo into a lecture or assign it as a shareable link — no lab installs.
- Do I need to install anything?
- No. It runs in any modern browser, free, with no account required.