Orion 2 - Research CubeSat

Orion 2 is a state-of-the-art CubeSat designed for low Earth orbit operations, featuring a modular payload system that allows for a wide range of scientific missions. This CubeSat is equipped with advanced sensors, high-resolution cameras, and communication systems that enable it to perform tasks such as Earth observation, atmospheric studies, and space weather monitoring. Its compact design and efficient power management make it an ideal platform for educational institutions and research organizations looking to conduct space-based experiments.

Project Specifications

Launch Mass 6.5 kg
Dimensions 60x20x20 cm
Power Solar panels with rechargeable batteries
Communication UHF/VHF radio link
Design Life 1 year

Download Resources

Research Opportunities

Apply for payload time on the Orion 2 mission.

Assembly Process Gallery

Chassis Integration
Chassis Integration
Solar Panel Deployment Test
Solar Panel Test
Thermal Vacuum Chamber
Thermal Vacuum

Mission Lifecycle & Goals

architecture

Concept & Design

Defining scientific objectives and payload requirements for Low Earth Orbit (LEO) experiments. The modular architecture is finalized to support diverse sensor arrays.