Bus

Structure & Mechanisms

Primary/secondary structure, deployment mechanisms, launch vehicle interface.

Bus

Electrical Power System (EPS)

Solar arrays, battery systems, power conditioning and distribution.

Bus

ADCS

Star trackers, sun sensors, reaction wheels, attitude control algorithms.

Bus

TT&C / Communications

S-band transponder, antennas, RF chain for deep-space communication.

Bus

On-Board Computer / Avionics

Flight computer hardware and flight software, including FDIR.

Propulsion

Propulsion System

Bipropellant thrusters, tanks, and hazardous-propellant qualified hardware.

Payload

PMS (Primary Science Instrument)

Dual-band microwave radiometer for lunar surface science.

Payload

Radiation Dosimeter

Secondary payload monitoring the radiation environment in cislunar space.

Payload

Narrow-Angle Camera

Imaging payload for outreach and mission documentation.

Test & Launch

AIT / Environmental Test Services

Vibration, thermal-vacuum, and EMI/EMC test facilities and execution.

Test & Launch

Launch Services

Launch vehicle integration and campaign support.

Mission & Ground

Ground Segment / DSN Access

Deep-space antenna time and ground station infrastructure.

Partner application

Tell us which subsystem(s) fit your capability — select as many as apply.