northrop grumman

structural engineering intern

to protect company proprietary information, diagrams shown below do not accurately portray hardware

💼 Overview:

Developed flight hardware and tooling for fast-paced programs such as Class-C military communication satellites and Air Force Research Lab (AFRL) proposals.

Intern in the Mechanisms and Deployable Products department

â›” Problems:

  1. Technicians were complaining that applying dry film lubrication (DFL) to flight-hardware threads was too time consuming and laborious.
  2. Classified program needed a way to characterize the parasitic torques generated within a satellite biaxial gimbal in order to inform the design of guidance, navigation, and control (GNC) algorithms
  3. Unclassified program urgently needed a 3D CAD model of their entire spacecraft for several reasons:
    • to provide the customer (Air Force Research Lab) with a visual rough concept
    • to verify systems requirements
    • to ensure smooth integration of subsystems developed by industry partners Westinghouse and Astrobotic

🔧 Work done:

  1. Designed 7 tooling setups in CATIA V5 to expedite the dry film lubrication process on flight hardware threads.
  2. Conducted experiments to characterize parasitic torques within a satellite biaxial gimbal. Ran ~100 tests on the azimuth and elevation axes. Created a MATLAB script to interpret and graph raw data collected by a custom-made testing computer. Created PowerPoints and presented torque data to GNC and Mechanisms engineers.
  3. Responsible for the system level CAD design of an experimental spacecraft. Came up with notional designs for payload locking mechanisms, hinges, cooling systems, and electrical harness routing. Saved the program ~$500k – $1M by reusing certain geometric features from another Northrop spacecraft.
  4. Participated in cross-company meetings where I pitched flight-hardware design changes to engineers at Westinghouse and Astrobotic.