Autonomous labs in space for

[MICROGRAVITY]

[ PRODUCTS ]

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.

Space-Based AI Processing

Advanced onboard analytics and decision-making.

Deep Space Missions

Supporting long-duration interplanetary exploration.

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 Al & 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

Mass of System:

380gm

Mass of Sequencer:

160gm

Payload Mass:

~3.5kg (Maximum)

Payload cf envelope:

X-Axis 80mm, Y-Axis 80mm, Z-Axis 120mm (from the base)

Hold down and release mechanism:

Burn Wire

Separation Velocity:

1 m/s to 3 m/s (configurable)

Operating Temperature:

-15 C TO +60 C

Compatibility:

Every Launch Vehicle

Standard:

Cubesat NextGen

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.

[ CONTACT ]

Collaborate with us on the future of space

Whether you're looking to partner, launch your payload, or just learn more, our team is ready to help. Reach out and let’s build the next frontier together.

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