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Specific Impulse Converter

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Specific impulse scale

350.0 s

The existing engine and reference scale connects specific impulse in seconds with effective exhaust velocity.

Effective exhaust velocity3,432 m/sIsp in seconds converts directly through ve = Isp × g₀low chemical / cold gaselectric propulsion350.0 s

Isp is exhaust velocity divided by g₀

Seconds can feel abstract, so the diagram keeps the equivalent exhaust velocity visible. Higher Isp means more impulse per unit propellant flow, not necessarily more thrust.

Specific impulse
350.0 s
Exhaust velocity
3.432 km/s
Thrust per mass flow
3,432 N/(kg/s)
Category
Good Performance
Common reference points
Cold Gas Thruster150 s
Hydrazine Monopropellant230 s
LOX/RP-1350 s
LOX/LH2450 s
Hall Thruster1,500 s
Ion Engine3,000 s

Performance category

Good Performance

LOX/RP-1, LOX/LH2, Most bipropellants

Specific impulse

350.0 s

Standard gravity-based unit

Effective exhaust velocity

3,432.3 m/s

3.432 km/s

Thrust per mass flow

3,432.3 N/(kg/s)

11,260.9 ft/s equivalent

Open Source and Easy to Use Elsewhere

This tool is open source and the underlying logic is fully transparent. You can inspect the code, understand the calculations, and contribute improvements. If you want to use the tool in your own website, course page, or learning platform, you can also embed it directly and start from a ready-made iframe setup for this exact tool.

Open source: review the implementation and see how the results are produced.

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