Skills necessary
Structure Design
Stress Analysis
Heat Transfer
Compressible Flow Analysis
Finite Element Analysis
Computer-Aided Design
Interface Control Models & Drawings
Prototyping
Programming
Team Collaboration
Test Planning
Delta Spaceship
SUMMARY
Led and Designed Secondary Fluid Systems and Structures for Delta Spaceship. Also worked on Avionics and Mechanical Design for Avionics and Interiors. Project is still on-going.
Public Information Link
Delta Space Ship
Responsibilities:
Created clean sheet designs for Delta Propulsion Design program
Created 3D CAD models and 2D drawings for Propulsion Detail Parts, Assemblies, and Installations with CATIA 3DX
Created Designs with GD&T per ASME Y14.5-2009, ASME Y14.5-2019, and ASME Y14.47 standards
Resolved Integration challenges of Propulsion System with the interfacing subsystems of Delta Spaceship
Developed and Documented system requirements and Interface Control Models for components and Integrated Systems
Created free-body diagrams and performed hand stress calculations for preliminary designs
Performed Thermal, Structural, and Fluid Analyses for Predicting Component Performance for Propulsion System
Performed FEA analysis using FEMAP/NASTRAN for Static, Dynamic, and Shock & Vibe per MIL-STD-810
Collaborated with Manufacturing, Testing, Materials & Processes, Avionics, Fuselage, Stress Analysis, and Systems teams to assure Hardware Producibility
Collaborated with Testing and Analysis to Determine Proper Pressure Budget and Model Adjustments for Production using Microsoft Visio and Python
Designed Systems that ensured Propulsion Safety Critical parts were Electrically Bonded per NASA-STD-4003
Created Tolerance Stackup Analyses to ensure parts and assemblies fit together even under worst-case scenarios
Supported verification activities to ensure that the propulsion system meets requirements
Supported review of manufacturing plans and procedures to ensure compliance with the requirements
Coordinated with Analysis and Mission Systems to ensure component performance in flight environments
Supported components throughout full lifecycle from prototype to final acceptance as well as modifications and repairs
Evaluated manufacturing issues and supported Non-Conformance Reports