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Bi-Liquid LOX/Ethanol for Precise, Reliable Thrust |
- High-Level Rocket Structure: Thrust Range, Vehicle Mass (+-50%)
- Conservative(High-Thrust) Thruster / Feed System Design + Review
- Fluid System Assembly, Testing, Calibration. Instrumentation and Control Development. Flight Structure Design Integration
- Static Fire Testing. Mass Optimization, Simulation Refinement.
- Flight Vehicle Integration
Priorities: Stable, Conservative Performance and Efficient Manufacturing/Assembly
- Injector: Unlike-Doublet Impinging, LOX-centered
- Chamber: Ablative + Fuel Jetted Wall-Film. 6061 Aluminum Jacket.
- Nozzle: Graphite Throat, 316L Stainless Steel Expansion
Image of Thruster & Injector Parts
Fluid System Piping and Instrumentation Diagram (P&ID)
Feed System CAD
Main Valves: Compact Pneumatic Linear & Rotary Actuators