Biprop Thrusters

A bipropellant thruster (Biprop), is a thruster that uses a liquid fuel and oxidizer to generate thrust. This specific thruster uses Hydrazine and Nitrogen Tetroxide to cause a hypergolic reaction.

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2 standard Bi-Propellant thrusters are currently available.

5N thrust

• 200 PSI target chamber pressure​

• 285s vacuum ISP

• 70mm overall length

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10N thrust

• 200 PSI target chamber pressure

• 290s vacuum ISP

• 80mm overall length

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Datasheets and models coming soon