Units

Propellant Properties

Grain Geometry

Nozzle Specifications

Simulation Controls

Advanced Settings

Max Thrust

-- N

Total Impulse

-- Ns

Burn Time

-- s

Max Pressure

-- MPa

Average Pressure

-- MPa

ISP

-- s

Propellant Mass

-- kg

Propellant Length

-- mm

Volume Loading

-- %

Initial KN

--

Peak KN

--

Ideal Thrust Coefficient

--

Delivered Thrust Coefficient

--

Throat/Port Ratio

--

Peak Mass Flux

-- kg/m²s

Quick Help

Propellant Properties

Enter the physical and chemical properties of your propellant. These values determine how the propellant burns and generates thrust.

Grain Geometry

Select and configure the shape of your propellant grain. The geometry affects the burn surface area and thrust profile.

Nozzle Design

Configure your nozzle dimensions. The nozzle converts high-pressure gases into high-velocity exhaust to generate thrust.

Need More Help?

Visit the documentation for detailed explanations and tutorials.