CubeSat Design

Antenna Deployer Module

Mechanism responsible for deploying the communication antenna once the spacecraft reaches orbit. Ensures reliable data transmission by extending the antenna into its operational position.

Specifications:

Communication Board

Handles the transmission and reception of data between the spacecraft and ground stations. Includes RF circuits and interfaces with antennas.

Specifications:

Camera and Lens

Captures visual data of Earth or space for imaging missions. Mounted with a lens and connected to the onboard computer for data processing.

Specifications:

Solar Panel

Provides electrical power to the spacecraft by converting solar energy into electricity. Essential for sustaining long-term operations in orbit.

Specifications:

Structure

The physical framework of the spacecraft that houses and supports all subsystems and payloads. Designed for mechanical stability and efficient thermal management.

Specifications:

Kill Switch and RBF Pin

A safety mechanism used during ground operations to prevent accidental activation of spacecraft systems. The Remove Before Flight (RBF) pin must be pulled prior to launch.

On-Board Computer

The central processing unit of the spacecraft. Manages control, communication, payload operations, and interfaces with all other subsystems.

Specifications:

Electrical Power System

Manages power generation, storage, and distribution onboard. Regulates voltage and supplies power to all systems using solar panels and batteries.

Specifications: