LIA Aerospace develops green, non-toxic bi-propellant propulsion systems for small satellites and spacecraft. Their accelerated manufacturing process delivers solutions in six months, enabling efficient orbital maneuvering and last-mile delivery with reduced environmental impact.
Funding
Funding not disclosed
Founders
Product
Problem
The space industry faces challenges with the cost and environmental impact of traditional propulsion systems. Current solutions often involve toxic or cryogenic propellants and lengthy manufacturing processes, limiting accessibility and sustainability for satellite deployment and orbital maneuvering.
Solution
LIA Aerospace provides green, non-toxic, and non-cryogenic bi-propellant propulsion systems designed for the last-mile delivery and maneuvering of small satellites and spacecraft. Our approach significantly reduces manufacturing and testing timelines, bringing products to market in six months compared to the industry standard of twenty-four months. This accelerated development cycle, combined with the use of safer propellants, makes space missions more accessible and environmentally responsible. Our systems are engineered for high Delta-V requirements, enabling efficient orbital changes and unlocking access to any orbit for the burgeoning New Space sector.
Target Audience
Our primary customers are satellite manufacturers, launch service providers, and companies developing small satellite constellations and in-orbit servicing platforms that require efficient and sustainable propulsion solutions.
Features
- Bi-propellant propulsion systems utilizing non-toxic, non-cryogenic propellants such as Hydrogen Peroxide (HTP) and hydrocarbon fuels.
- Accelerated manufacturing and testing processes, enabling product delivery within six months.
- High specific impulse (ISP) of 320 seconds and thrust capabilities up to 715N.
- Thrust Vector Control (TVC) with gimbaling up to ±10° for precise attitude control.
- Integrated cold gas Reaction Control System (RCS) for roll control and pre-burn stabilization.
- Designed for high Delta-V missions, facilitating orbital changes and last-mile delivery for small satellites.
- Adaptable for launch vehicle kick stages, potentially increasing small launch vehicle capacity by up to 70%.
- Suitable for lunar and Mars landers requiring controlled descent and translational maneuvers.
- Available in BP100 and BP200 configurations, supporting payloads up to 15" and 24" respectively.