Skip to end of metadata
Go to start of metadata

You are viewing an old version of this page. View the current version.

Compare with Current View Page History

« Previous Version 6 Next »

Team Members:


Project Mission:

RL-36 is Launch Initiative’s first liquid bipropellant rocket engine. The engine is a reaction control system (RCS) that can be implemented for trajectory and attitude control of a space vehicle. The thrust is 36 lbf, which is in the thrust range of RCSs for small satellites. Like most auxiliary engines, RL-36 uses a gas pressure-fed, blow-down feed system. The project is a test platform for future liquid engines that the team plans to integrate into competition rockets.


Expected Timeline:



Project Pages:

  • No labels