Functional Test

Functional Test Components

• Battery Pack

• PCU

• Solar Wings

• CDH

• ADCS

• GNSS

• Star Tracker

• ADCS Sensors

• Payload / Payload Stand-In

Functional Test Sequence

During the full functional test, the bus is connected to a computer with the flight software code. for debugging purposes. The satellite is turned on after 100s hold mode using the power supply. At this stage, the PCU will be turned on to distribute power to other subsystems. A command is sent to CDH subsystem to deploy the solar wings. Any telemetry and data can be acquired various sensors and boards through the umbilical cord upon flight software commands.

Reduced Functional Test

Reduced Functional Test Components

• Battery Pack

• PCU

• CDH

• ADCS

• GNSS

• Star Tracker

• ADCS Sensors

• Payload

Reduced Functional Test Sequence

Reduced functional test will repeat the full functional test activities without deploying the solar wings.

More details will be added to this page during phase D.