# Autonomous Labs in Space for

# [MICROGRAVITY]|

## End-to-End Space Infrastructure Under One Roof.

The only company in the world, from the tip of the rockets (deployers) to spacecraft to data (ground stations), fully vertically integrated.

## Cosmotron

The Cosmotron is a 50 kg class, fully vertically integrated spacecraft platform designed for rapid deployment in various space applications.

Fully Integrated Platform

- Consolidates OBC (On-Board Computer), EPS (Electrical Power System), Communications, and Edge Computing onto a single PCB.
- Reduces weight, complexity, and launch costs.

### Flexible Payload Interfaces

- Supports both hosted and dedicated payloads.
- Designed for scalability and modularity.

### AI-Driven Edge Computing

- Enables real-time data processing in space.
- Supports advanced AI algorithms for mission autonomy.

### High-Speed Communication

- Ensures efficient data transfer for space applications.
- Supports low-latency connectivity.

Applications:

### Technology Demonstration

- Validating new space technologies.

### Earth Observation

- High-resolution imaging and remote sensing.

### Scientific Research

- Supporting microgravity experiments and deep space studies.

## Designed for the New Space Economy!

The Cosmotron Bus offers a scalable, modular, and cost-effective solution for emerging space missions, making it a versatile choice for commercial, scientific, and exploratory endeavors.

- **Class:** Quarter Plate  
- **Spacecraft Mass:** 50kg  
- **Payload Capacity:** 20-30 kg  
- **Payload Volume:** Modular  
- **In-Orbit Average Power:** 100W  
- **Bus Voltage:** 5V, 12V, 32V (Customization Available)  
- **Pointing Accuracy:** <100" (3-sigma)  
- **Standard In-Orbit Demo Duration:** 6 months - 1 year  
- **Data Storage:** 64GB EDAC-protected  
- **Edge Computing:** Onboard GPU for AI & data processing  
- **Communication:** UHF, S-Band, X-Band  
- **Data Rates:** Up to 10 Mbps Downlink & Up to 1 Mbps Uplink  
- **Payload Interfaces:** CAN, RS422/RS485, UART, Ethernet, I2C, SPI (Customization Available), SpaceWire

### Class: 0.5m class  
- **Mass:** 27kg  
- **Payload Mass:** 5kg  
- **Payload Volume:** 4U (Pressurized)  
- **Maximum Entry Gs:** <15  
- **Communications:** Iridium  
- **Mission Duration:** <3 Months

## REX(50)

## REX(100)

REX (100) features a viewport for plasma dynamics observation during hypersonic atmospheric reentry and precision capsule delivery using guided parafoils.

- **Class:** 1m class  
- **Mass:** 85kg  
- **Payload Mass:** 10kg  
- **Payload Volume:** 12U (Pressurized)  
- **Maximum Entry Gs:** <15  
- **Communications:** Iridium  
- **Mission Duration:** 3-6 Months

## DEPLOYER-X

DeployerX is a non-canisterised, pin-based separation system developed for nanosatellites. It follows our in-house developed next-generation CubeSat standard (CubeSat NG), allowing customers to benefit from a lighter separation system mass. This results in lower launch costs and the ability to accommodate unrestricted volume in satellite structures.

## Let's Do This.

Just talking won't get you to space, action will. We've done it 26 times already, one more won't hurt. If you're serious, we should talk.

2 Marina Blvd B300, San Francisco, California 94123, US.