Try an example search:x-bandcubesatbatteryOr file a request and let us do the work!

10N Bipropellant Thruster S10-13


The 10N bipropellant thruster is a small rocket engine that uses the storable propellants monomethylhydrazine MMH as fuel and pure di-nitrogen-tetroxide N2O4, or mixed ox-ides of nitrogen (MON-1, MON-3) as oxidizer. It is designed for both, long term steady state and pulse mode operation. It operates in a wide pressure range at regulated pressure as well as in system blow down mode with flight heritage down to 6 bar inlet condition. Combustion chamber and nozzle are made of platinum alloy that does not need any surface coating. It allows operational temperatures up to 1.500°C (2700°F) and thus maximum thruster performance.


mass350 g
full datasheet


Submitting your information allows us to get in touch with you once we get a response from the supplier.

I am interested in*:

Would you like suggestions about similar products from other suppliers?  

Requests that are submitted through satsearch are anonymously posted to our leads page.

Disclaimer: satsearch is not responsible for any mistakes on this page, although we do our best to ensure correctness. Please report any mistakes to us.

Last updated: 2019-07-17