Prototype Development & System Design
Completed Design: Human Landing System (HLS)
Developed detailed engineering prototype with comprehensive system integration including:
Cutaway Model Architecture - Engineered sectional model revealing internal systems layout and component integration Life Support System - Integrated compact environmental control and life support system (ECLSS) with redundancy protocols Autonomous Docking Interface - Designed docking mechanism compatible with Lunar Gateway and crew transportation vehicles Gateway Staging Operations - Planned orbital staging procedures and deployment sequence from Gateway Propulsion System - Developed compact propulsion architecture with optimized fuel efficiency and throttle control Electrical Power System - Configured power generation, storage, and distribution network for all mission phases Radiation Protection - Incorporated multilayer shielding architecture for crew protection during lunar operations GN&C Integration - Integrated Guidance, Navigation & Control suite with precision landing and hazard avoidance capability LunaNet Communication - Implemented communication architecture for real-time data relay and network connectivity
Technical Documentation & Deliverables
Project Outputs:
Comprehensive technical research documentation covering mission-critical subsystems Fully annotated engineering prototype with dimensional specifications and materials analysis Cutaway visualization illustrating internal systems integration and operational interfaces Design rationale report detailing engineering trade studies and optimization decisions Technical presentation synthesizing mission requirements, design solutions, and system capabilities
Project Coordination
Assigned and coordinated team roles across research, design, and documentation phases. Managed resource allocation, technical review cycles, and prototype development timeline. Ensured all preliminary design review deliverables met NASA mission requirements and engineering standards