"Future is here"
​Ophio OI
The Ophio-01 represents a leap forward in space travel technology, utilizing fusion power to extend missions beyond traditional limits and enhance sustainability
Core Propulsion & Performance
• Propulsion System: Ophio-CFR-1 Compact Fusion Reactor. Utilizing D-He3 (Deuterium-Helium-3) aneutronic fusion for high safety and energy efficiency.
• Thrust Mechanism: Magnetic Plasma Jet Thrusters (MPPT). Achieves stable thrust exceeding 100,000 N (Newtons) with extremely high Specific Impulse (Isp).
• Maximum Velocity: 50,000 km/h. Capable of rapid ingress and adjustment within near-Earth orbit; acceleration to LEO (Low Earth Orbit) takes only 20 minutes.
• Endurance: No refueling required within the design lifespan. The extreme efficiency of fusion fuel (Deuterium and Helium-3) allows for continuous power provision throughout its operational cycle.
• Energy Output: 1.2 GW (Gigawatts) net power generation. Output powers not only the thrusters but also onboard systems, payload, and future orbital infrastructure.
II. Vehicle Structure & Mission Capability
• Vehicle Dimensions: Length: 45 m / Width: 18 m / Height: 12 m. Compact design for compatibility with multiple launch vehicles and optimized maneuverability for orbital operations.
• Payload Capacity: Maximum payload: 50 Metric Tons. Capable of transporting large satellites, orbital resupply modules, or supporting heavy orbital construction.
• Orbital Altitude: LEO from 300 km to 2000 km. Capable of rapid adjustment between various orbital altitudes to perform diverse missions.
• Protection System: Plasma Shield and Intelligent Thermal Management System. Effectively defends against space debris, micrometeoroid impacts, and extreme thermal variations.
• Primary Missions: Heavy orbital transport, space debris removal, modular space station construction, and potential for ultra-high-speed point-to-point transport. The low-cost, high-frequency transport capability enabled by fusion power is its core value.
