The 28V Point of Load regulator is designed to allow missions with a higher bus voltage to utilize lower voltage components, without needing to change the spacecraft EPS design, or run long, low-voltage harnesses.

The MPPT connects the Solar Arrays with the battery, making sure that energy flows smoothly into the system, and operates at peak efficiency at all times.

The MPPT connects the Solar Arrays with the battery, making sure that energy flows smoothly into the system, and always operates at peak efficiency.

The Load Controller is responsible for switching on/off the supply of power to all the modules on the spacecraft, as well as providing primary actuation for torque rods, and gathering temperature data from thermistors not otherwise part of a module.

The 6-cell body mount panel is used on Terran’s larger microsat platforms, generating power to fuel the mission.

The Nano Solar Array is Terran’s standard nanosat class solar array, used in 6U spacecraft and above. The array uses a tri-fold design, allowing it to collapse into a very small volume, compliant with most 6 and 12 U dispensers.

Backplanes are the arteries of a spacecraft, connecting all components in the spacecraft together. The Mavericks Bus Backplane is the standard backplane used for the Mavericks platform but can be customized for various mission needs.

The SADA Stand-In Module provides mounting fixtures and harness routing to externally deployable solar arrays on missions that do not require the SADA module

The RWA combiner board allows Terran Orbital to construct compact triads of reaction wheels for additional redundancy.

The Load Controller is responsible for switching on/off the supply of power to all the modules on the spacecraft, as well as providing primary actuation for torque rods, and gathering temperture data from thermistors not otherwise part of a module.

Our 66V system increases the base voltage supplied to different parts of the spacecraft, ensuring that as our systems and power needs grow larger, efficiencies stay high

The 28V Point of Load regulator is designed to alow missions with a higher bus voltage to utilize lower voltage components, without needing to change the spacecraft EPS design, or run long, low voltage harnesses.