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SpaceX

During my first co-op at SpaceX, I worked with a team of Manufacturing Engineers for Dragon Propulsion. I was responsible for the manufacturing of the Crew Dragon high-pressure propellant abort system including process design for orbital tube welding and pressure testing as well as laser scan inspection, defect analysis, and tooling design.

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I also worked on several process improvement projects to save the company money as more capsules are produced through the use of custom tooling and equipment. 

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Tools Used: NX, Teamcenter, GD&T, Ansys, 3D Printing

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Note: All images are sourced online and are only to provide visual aid to descriptions.

SpaceX Crew Dragon Capsule ISS.jpg

Tooling Design

The Problem

  • During welding of large tubing assemblies off the capsule, the ends have high amounts of deflections which prevents assembly mating on the capsule

  • It is costly to cut and re-weld tubes on the capsule and there is risk of introducing foreign debris into the tubes which can ignite with the hypergolic fuel

  • Ends must be less than .005” out of tolerance on several 6’ long tubing assemblies


Solution

  • 2 dozen tools were modeled in NX to mimic the end constraints of the capsule as well as constrain the tubing and flanges during welding

  • Tools allowed multiple assemblies to be welded at the same time on the same table

  • Utilized GD&T to create drawings and outsource the parts for machining


Result

  • Tooling was used for building future capsules

  • There was no deflection when mating the assemblies using the tooling on the capsule

SpaceX Crew Dragon Jetpack Super Draco.jpg

SuperDraco Tubes I worked On

GD&T SpaceX.png

Example of Drawings Created

Defect Analysis

The Problem

  • During welding and bending of tubes, the ends may be out of tolerance compared to the drawings and there may be weld defects

  • Tubes and assemblies need to be bent into place when installed on the capsule which introduces additional stresses into the lines

  • Weld defects introduce stress concentrations at joints

  • Need to find out if the additional stress causes the tubing to fail during use


Solution

  • The tubing assemblies were laser scanned into NX and compared with the CAD models to determine the amount of displacement at the ends

  • ANSYS models were created for tube ends to calculate the stress of bending the tubes back in place

  • Welds were x-rayed to check for defects

  • ANSYS models were created for weld defects to characterize the KT factors compared to a nominal weld


Result

  • Lines that would not yield were kept and lines that would yield were remade

  • KT models were created for certain conditions to be referenced by other engineers

SpaceX Laser Scan.png

Example of Comparing Scan Data

Spacex Ansys.jpg

Example Ansys Model

Process Optimization

The Problem

  • K seal ports need to be polished to a high surface finish for sealing and it can take over a day to complete one port by hand 

  • There are over a thousand port surfaces on a capsule which takes up a lot of technician time


Solution

  • A custom rotary tool with a 3D printable frame was designed in NX to increase the rate at which ports can be polished and to be able to get into tight corners in assemblies

  • A set of polishing adapters were created to be used on all types of ports and interface with the rotary tool

  • Utilized GD&T to create drawings and outsource the parts for machining

  • Performed polishing studies and statistical analysis to ensure that they were safe for part use 


Result

  • One port could be polished in minutes comparted to the hours it would take previously

  • Tools were used deemed to be safe for use and were implemented into the polishing process

SpaceX AS5202 Port.jpg

K-Seal Port

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