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James Webb Space Telescope propulsion subsystem

The James Webb Space Telescope propulsion subsystem combines four Secondary Combustion Augmented Thrusters (SCATs) using hydrazine and dinitrogen tetroxide for major orbit-correction and station-keeping maneuvers with eight hydrazine-only MRE-1 thrusters for attitude control and reaction-wheel momentum unloading. NASA and STScI document the two thruster classes and their spacecraft functions; the exact manufacturer or finer model lineage of the SCAT hardware is not asserted here.

Identity

Aliases
JWST propulsion subsystemWebb propulsion system
Domains
spaceflight
Identity Level
integrated-system
Kind
integrated-propulsion-system
Name
James Webb Space Telescope propulsion subsystem
Status
active

Details

Description
The James Webb Space Telescope propulsion subsystem combines four Secondary Combustion Augmented Thrusters (SCATs) using hydrazine and dinitrogen tetroxide for major orbit-correction and station-keeping maneuvers with eight hydrazine-only MRE-1 thrusters for attitude control and reaction-wheel momentum unloading. NASA and STScI document the two thruster classes and their spacecraft functions; the exact manufacturer or finer model lineage of the SCAT hardware is not asserted here.
Propellants
hydrazinedinitrogen tetroxide

Links

Assets & Meta

Creation Time
September 7, 2026 at 21:49:28 UTC
Updated Time
September 7, 2026 at 21:49:28 UTC

Other

Search Name
James Webb Space Telescope propulsion subsystem JWST propulsion subsystem Webb propulsion system
Sources
James Webb Space Telescope propulsion subsystem - AeroVia