Relativity Space designs and manufactures medium-to-heavy lift reusable rockets using advanced 3D printing technology, enabling rapid production and reduced complexity in rocket development. The company addresses the growing demand for commercial launch services by providing cost-effective solutions for satellite deployment into various orbits.
Funding
$2M raised to dateRaised to date based on public sources. This may differ from the amount the company actually raised and is based only on what is publicly available on the internet.
+9Founders
Product
Problem
The increasing demand for commercial launch services is outpacing the available supply, creating a need for more cost-effective and rapidly produced launch solutions. Traditional rocket development is often slow and complex, hindering the ability to meet the growing need for space infrastructure and satellite deployment.
Solution
Relativity Space addresses this challenge by designing, manufacturing, and launching medium-to-heavy lift reusable rockets using advanced additive manufacturing techniques. This approach enables rapid iteration, reduces vehicle complexity, and lowers production costs compared to traditional methods. Their primary launch vehicle, Terran R, is designed for reusability and optimized for deploying customer satellites into various orbits. By leveraging 3D printing and an iterative development process, Relativity Space aims to provide commercially competitive launch services and unlock new value in the space economy. The company is also investing in infrastructure to scale rocket design, testing, and manufacturing at an accelerated pace.
Target Audience
The primary target audience includes commercial satellite operators, government space agencies, and other entities requiring reliable and cost-effective launch services for deploying payloads into various orbits.
Features
- Additive manufacturing (3D printing) of primary rocket structures and integrated components
- Reusable Terran R launch vehicle designed for medium-to-heavy payloads
- Aeon R 3D-printed engines utilizing liquid oxygen/methane propellant
- Development and application of proprietary thermal protection systems (TPS) for atmospheric re-entry
- In-house design, manufacturing, and testing of critical components, including valves
- Horizontal integration facility at Launch Complex 16 for Terran R
- Hot fire testing of Aeon R engines with flight-like Integrated Propulsion System (IPS) at NASA Stennis
- Capability to launch 23,500 kg to Low Earth Orbit (LEO) with downrange landing
- Capability to launch 5,500 kg to Geosynchronous Transfer Orbit (GTO) with downrange landing
- Capability to launch 33,500 kg payload to LEO in expendable configuration