Owen Pavlock.

Aerospace Engineering · University of Michigan

I design, build, and test mechanical systems.

Most recently a tendon-driven robotic gripper at HIROTEC America. Right now, parachute recovery hardware for a student rocket and an ultraviolet imager headed for 90,000 ft.

Study
B.S.E. Aerospace Engineering, Minor in Business, 2029
Focus
Mechanical design, test, and systems engineering
Based
Ann Arbor, Michigan
CAD render of a three-finger robotic gripper on a round plate, each finger mounted on a linear rail driven toward a central hub
Fig. 1Three-finger end effector concept with radial rails, so the grip can open or close around parts of different sizes. Siemens NX.

01 · HIROTEC America, Summer 2026

A gripper that holds 5 to 20 kg parts of any shape

HIROTEC builds body-in-white tooling for automakers, and every new part shape usually needs its own custom end-of-arm tool. I pitched a flexible alternative: a three-finger, six-motor gripper whose fingers are pulled by tendons the way human fingers are.

As the sole project champion, I took it from requirements through verification, with intern support I directed. The design was presented to executives and the Japanese parent company, and it compared well against their own multi-month effort.

$11.2k
funding secured from the pitch
3 wks
ahead of schedule
$5k
under budget
Read the case study
CAD render of three jointed robotic fingers standing on a circular base plate
Fig. 2Finger assembly. Each finger has two joints driven by antagonistic tendon pairs.

Teams & coursework

Rockets, imagers, and aircraft

Reefed parachute and tether shock loads

Chutes & Tethers Responsible Engineer, Recovery

  • Leading a parachute and tether shock-load verification test, backed by a MATLAB dynamic model that predicts system response, to show structural integrity to 4,000 lbf for flight certification.
  • Designing a skirt-reefed main parachute that disreefs in stages, so one canopy replaces a three-parachute recovery system while keeping opening shock low.
  • Building a 6-DOF flight simulator in C++ on NASA's Trick and JEOD frameworks, including job scheduling, integration loops, and physics models for multiple rocket configurations.
lbf 0 400 800 1,200 1,600 A · REEFED DEPLOY, FROM APOGEE 384 lbf 0s 5s 10s 15s B · DISREEF TO FULL OPEN, FROM CUT 1,490 lbf 0s 1s 2s 3s
Fig. 3Opening shock from my Knacke-based MATLAB model of the single reefed canopy: a 383 lbm rocket, 24 ft canopy reefed to 7 ft at apogee and cut free at 1,000 ft. Early estimate with placeholder inputs; peak load leaves a 3.4× margin on the 5,000 lb bridle.

MAAX ultraviolet imager proof of concept

Risk Lead & Avionics, AEROSP 388

  • Lead risk management for a team using model-based systems engineering to scope UV imaging analysis for MAAX, a candidate NASA Heliophysics SMEX mission. I brief MathWorks and SPRL stakeholders every two weeks.
  • Defined objectives and requirements for analyzing auroral UV imagery from the MAAX Ultraviolet Imager (MUVI), and carried the design through several reviews to a baseline.
  • Integrating the lens, avionics, and camera for a weather balloon flight to 90,000 ft to prove the concept.

Sensor-payload rocket

Design Team Member

  • Took a sensor-payload rocket through design, build, integration, launch, and flight-data analysis, and defended it at a Preliminary Design Review and a Flight Readiness Review.
  • When the landing point drifted from what simulation predicted, I worked through the flight data and wrote the root cause analysis.

Airfoil and aircraft analysis

Aerodynamics Team Member

  • Ran airfoil and full 3D aircraft analyses in AVL and STAR-CCM+ to check the design against critical flight parameters and drag targets. The design changes that came out of it cut takeoff time by 20%.

Experience & education

Where I've been

2025 – 2029 University of MichiganB.S.E. Aerospace Engineering, Minor in Business · GPA 3.87 Ann Arbor, MI
May – Aug 2026 HIROTEC AmericaResearch & Development Intern, Robotic End Effector Project Champion Auburn Hills, MI
Expected 2027 INCOSE Systems Engineering CertificationInternational Council on Systems Engineering

Relevant coursework: Aerospace Structures, Dynamics & Vibrations, and the Space Systems MBSE project (AEROSP 388).

About

I like problems where the math has to survive contact with real hardware. At HIROTEC that meant learning from the first 3D-printed finger that our torque model was wrong, then building a load-cell rig to settle it. Outside engineering I follow finance and football, build websites, and play poker. I'm also part of AIAA's Professional Development Committee and 42 Strong.

Software & code

  • MATLAB
  • C++
  • Python
  • Arduino
  • Linux / Bash
  • Siemens NX
  • CadQuery
  • STAR-CCM+ (CFD)
  • AVL
  • NASA Trick / JEOD

Systems engineering

  • Model-based systems engineering
  • Stakeholder needs & requirements
  • Risk management
  • Design reviews (PDR, FRR)
  • Verification & test planning
  • System integration
  • Root cause analysis

Fabrication & hardware

  • 3D printing (FDM, TPU)
  • Machining
  • Soldering
  • Stepper motor control
  • Load cell instrumentation

Contact

Looking for internships in aerospace and robotics hardware.