NASA's Goddard Space Flight Center

Honeywell Aerospace

Jena-Optronik GmbH

European Space Agency (ESA)

Taber Industries

ABSL Space

ATK Space Systems

This the main body and structure that all other spacecraft pieces are attached to. It holds the electronics and equipment that support the telescope and instruments.

Observatory Support Systems

The six-sided primary structure, also called the spacecraft bus, provides the structural support for the observatory. It contains six compartments, or avionics bays, that house key electronics and components for running the rest of the spacecraft. It's made up of a central cylinder with a top deck that supports the rest of the observatory and a bottom deck that interfaces to the rocket during launch.

Primary Structure

The LISS consists of two deployable panels attached to the spacecraft bus, which are designed to help shield the observatory from sunlight.

Lower Instrument Sun Shade (LISS)

The ACS is a three-axis stabilized system that uses precision pointing to rotate the observatory to the right position for science. Six motorized flywheels, called reaction wheels, will enable the observatory to perform short, frequent movements to repoint at different regions of the sky required for science observations.

Attitude Control System (ACS)

The propulsion system will use hydrazine in its two types of thrusters to maneuver the observatory. Hydrazine is a monopropellant, which means it doesn't need a second chemical to combust – only contact with a catalyst. Roman will have enough fuel to operate for at least 10 years.

Propulsion

Solar cells on the solar array panels will convert sunlight into power to provide 4,100 watts to the observatory electronics while shading the spacecraft underneath it. This system includes a battery to regulate the voltage to all electrical components and provide back-up power when there is no Sun available to the solar array. This will not be used often because the observatory's orbit at L2 will keep it in full view of the Sun at all times.

Power

The C&DH system is responsible for monitoring the health and safety of the observatory. This includes collecting telemetry and housekeeping data, monitoring temperatures, sending out hardware commands. It will also store up to four terabytes of science data in its Science Data Recorder (SDR) for downlink to the ground when a ground station is in view.