MONARC 90 REM

The Rocket Engine Module (REM) 听is a unique configuration of three MONARC 90 thrusters, providing optimal performance for spaceflight applications. These thrusters, which consist of one axial and two 90 degree turn flow thrusters, are liquid monopropellant thrusters designed to operate with hydrazine. The REM is cleverly designed such that the thruster inlets are connected via a common manifold, establishing a singular inlet for the assembly. This arrangement aids in creating a compact, integrated system that has been thoroughly tested and proven in the field.

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Model Family / Configuration鈥�	MONARC 90 REM
笔谤辞辫别濒濒补苍迟鈥�	HPH (N2H4)
Components听听听	3 MONARC 90 Engines, Thermostats, Engine heaters and sensors, Connectors, Harnessing
Heritage Highlights	Space Launch System (SLS), 鈥�First flight on Artemis 3