K200 is the first flex-propellant solid jet engine, engineered for suborbital spaceflight, kinetic-kill CUAS, and hypersonic projectile launch. Nozzle geometry and pellet size/composition are tailored to the mission.
Maximum power output: 200 MW / 300,000 hp
Maximum solid jet velocity: 5,000 mps / 16,000 fps
Maximum thrust: 5,000 kgf / 11,000 lbf
Maximum pellet size: 10 mm / 0.4 in
Minimum solid jet divergence: 0.46 mrad / 1.6 arcmin
Maximum weight: 1,600 kg / 3,600 lbs
Length: 5 m / 16 ft
Energy source: Thermal battery, diesel/air torch
Thermal efficiency: 80% with propellant recycling
Propellant options: Air, hydrogen, methanol, diesel
Pellet options: Steel, clay, plastic, tailored energetics
