Rocket Science: Technical Specs

Propulsion System

Based on TBD-5000 turbofan engine, with a 1000kW power output.

Using Liquid Nitrogen as the primary oxidizer.

Estimated 5% efficiency boost in fuel consumption due to Advanced Ionized Plasma Injectors.

Nose Cone

Materialized in Tantalum-5 for maximum Heat-Resistant properties.

Diameter: 100mm with a 5° angle.

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