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Instrumentation, Control, and Communications: On the Ground and In Flight
Multi-Modal Design, Manufacturing for Advanced Aerostructures
Dual-Side Dual-Chute Deployment for Reliable, Condition-Tolerant Recovery.
STAR's 2nd ever stage separation vehicle! Competing in IREC 2024 in the 30k COTS category
Kinetically Engineered Life Support Experiment - Yeast
Compilation of all current projects that STAR is working on this academic year!
STAR's First Liquid-Powered Flight Vehicle
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 Perfomance 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
Team Development/Technology Capabilities
Rapid design iteration
Physics, Analysis-oriented testing
Efficient Cross-Specialty Collaboration
Development for Reliability, Robustness
Expand team technicality, individual learning capability
Target Apogee, Precision: 2500m, +-10%
Approx. Vehicle Mass: 40kg dry
Approx. Thrust Level, Burn Time: 1.80kN, 10sec