the Next Generation of Defense and Space

CycloJP is a high energy density replacement for conventional aerospace fuels, including Jet A, JP-5, JP-8, and JPTS, designed to enhance performance across both manned and unmanned aircraft platforms.

By significantly increasing energy density, CycloJP enables aircraft to fly farther and longer, extending mission range and endurance without additional fuel volume. Its advanced formulation also supports higher-altitude operations, with superior low-temperature performance and viscosity characteristics that maintain fuel integrity in extreme conditions.

Improved thermal stability enables more efficient high-speed flight, while cleaner combustion produces lower-luminosity flames and exceptionally lower soot emissions vs. Jet A, extending engine life and maintenance intervals.

CycloJP supports a wide range of mission profiles, including:

• Turbine-powered platforms, CCA, UAS and C-UAS
• Attritable systems
• Special missions, including high-altitude, long-endurance ISR platforms
• Next-generation high-speed propulsion systems

CycloRP is a high-performance, drop-in replacement for RP-1 and RP-2 kerosene-based rocket fuels, designed to improve launch efficiency and payload capacity. With significantly higher volumetric and gravimetric energy density, CycloRP enables launch systems to carry more payload without increasing fuel load, directly improving launch economics and cadence. These gains allow rockets to achieve the same energy output with less propellant loading, freeing capacity for substantial increases in payload mass per launch.

Superior thermal stability also improves regenerative cooling performance, supporting more efficient and reliable propulsion system operation in demanding launch environments. Cleaner combustion and lower soot emissions as compared to RP-1 and RP-2 extends engine life and maintenance intervals for reusable engines.

CycloRP is optimized for:

• Space launch platforms
• In-space propulsion

CK-10 is a next-generation replacement for JP-10, engineered to enhance the performance of long-range missile platforms. With improved energy density and combustion characteristics, CK-10 enables systems to fly farther and longer, extending effective mission range and standoff distance.

With improved energy density and combustion characteristics, CK-10 enables systems to fly farther and longer, extending effective mission range and standoff distance.

Its advanced formulation also supports high-speed performance and improved thermal stability, enabling propulsion systems to operate more efficiently under demanding mission conditions.

CK-10 is designed for:

• Long-range and high-performance missile systems