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Mechanical Engineering — Northeastern University

Sebastian
BujarskiHardware & robotics, drawn to spec

Four projects spanning soft continuum robotics, bistable structural research, near-space instrumentation, and renewable energy — designed in CAD, built by hand, and flown or tested to see if the theory held up.

DocumentFull Portfolio Set
Drawn byS. Bujarski
Sheets8, indexed above
Rev2026.2
GENERAL NOTES

About

B.S. MECHANICAL ENGINEERING

I'm a mechanical engineering student at Northeastern, drawn to the parts of a project where a sketch has to become a physical thing that actually works — a joint that has to bend without binding, a fixture that has to hold a sample true, a payload that has to survive a 100,000 ft drop back to earth.

Right now that means undergraduate research in the Transformative Robotics Lab under Professor Jeffrey Lipton, characterizing bistable structures, alongside coursework in CAD, robotics, and statics. Outside the lab: three years as Senior Patrol Leader working toward Eagle Scout, four years running shifts at a local restaurant, and current volunteer work with the Lyme Fire Department.

SchoolNortheastern Univ.
DegreeB.S. ME
MinorAerospace Eng.
Expected2029
BILL OF MATERIALS

Skills

TOOLS & METHODS
ItemCategorySkillNotes
01CAD & DesignSolidWorksCSWA in progress · primary CAD across all three projects
02CAD & DesignOnShapeCloud CAD, secondary tool
03ProgrammingC++Embedded sensor systems — HAB ozone module
04ProgrammingPythonData handling & scripting
05ProgrammingHTML / CSSBuilt this page
06Fabrication3D PrintingTrunk segments, BETR unit cells & test fixture
07FabricationLaser CuttingBETR sheet-metal unit cells
08FabricationWeldingWelding Merit Badge (BSA) · informal practice, Makerspace
09ElectronicsArduino / Raspberry PiControl & telemetry across projects
10LeadershipProject & team managementLed teams of 3–8 across research, class, and volunteer projects
PROJECT SHEET 1 OF 4 — ZONE B2

The Trunk

BUILT & DEMOED

A soft continuum robotic arm inspired by an elephant's trunk, built for Cornerstone Engineering II with teammates Yonas and Karl. The arm has two independently bendable sections, each pulled by four tensioned strings routed through a stack of 3D‑printed disk and spool segments — so each section curls in any direction depending on which strings are pulled taut.

I modeled and dimensioned the disk and spool components in SolidWorks (drawings at right), sized so string channels stayed aligned through the full range of bending without binding. Four DC gearmotors per section, housed in a wired control base, act as winches to pull the strings; an onboard LED strip marks which segment set is active.

Bendable sections2
Strings / section4
Disk OD2.00 in
Winch motors8
Team size3
Fabrication3D print
ROLE — Designed & dimensioned disk/spool segments in SolidWorks · built & wired the winch base · assembled the string-actuated arm
The Trunk arm lit up on a demo table
FIG. 1 — segment assembly during a live demo, LED strip marking the active string set
SolidWorks drawing of the disk component
FIG. 2 — disk, Ø2.00" · SCALE 1:1
SolidWorks drawing of the spool component
FIG. 3 — spool, Ø.75" · SCALE 4:1
Top-down view of assembled trunk segments
FIG. 4 — segment sets labeled top/bottom pre-assembly
Winch control base with motors and wiring
FIG. 5 — winch base: 8 gearmotors, breadboard control circuit
PROJECT SHEET 2 OF 4 — ZONE B3

BETR Cylinder

TRL LAB RESEARCH

Ongoing research with Northeastern's Transformative Robotics Lab (TRL), under Professor Jeffrey Lipton, alongside graduate students and a collaborating professor's group abroad. The project builds a bistable, radially-expanding hexagonal structure — a "2.5D" cylindrical form made of repeating chevron unit cells that snap between a compact and an expanded state as the cylinder is extended vertically.

The graduate team fabricates the unit cells several different ways — laser-cut from a few different materials, and 3D-printed in a few different materials — to see how fabrication method and material change the bistable response. My role has been testing and characterizing those units: manual measurement, motion-capture-tracked deformation, straightforward visual/qualitative testing, and full stress-strain characterization on an Instron tensile tester.

To make that Instron testing possible, I designed and fabricated two things myself: a small connector piece that joins each end of a unit cell together, and a mounting fixture that clamps a test sample into the Instron and lets it rotate freely as it deforms (the CAD model and sketch at right). The resulting stress-strain curves show the repeated snap-through peaks that give each layer its "click" between states, feeding results back to the team's next design pass.

BehaviorBistable
ExpansionRadial
GeometryHex chevron unit
Materials (team)Print · steel · fabric
Testing methodsManual · Instron · mocap · visual
My fabricationEnd connector + Instron fixture
ROLE — Tested & characterized unit cells fabricated by the grad team (manual, Instron, motion-capture, visual) · designed & fabricated the end connector and Instron test fixture · fed results back into the design loop
Assembled bistable hexagonal cylinder structure
FIG. 1 — assembled cylinder, repeating chevron units in the expanded state
Single rigid 3D-printed bistable unit cell
FIG. 2 — single unit cell, 3D-printed rigid iteration (grad team fabrication)
Flexible fabric composite version of the unit cell
FIG. 3 — flexible fabric/composite iteration of the same unit (grad team fabrication)
Slicer software layout of unit cells on a 3D printer bed
FIG. 4 — unit cells arranged for a print run
Nested laser-cutting layout of unit cells
FIG. 5 — nested layout for a full sheet, laser-cut variant
Sheet of laser-cut unit cells ready for assembly
FIG. 6 — cut sheet, ready to fold & assemble into a cylinder
CAD model of the four-arm Instron test fixture
FIG. 7 — Instron test fixture, modeled in SolidWorks
3D-printed test fixture held in hand
FIG. 8 — the printed fixture, ready to mount a sample
Structure surface marked with motion-capture tracking dots
FIG. 9 — motion-capture markers tracking surface deformation under load
Stress-strain graph showing repeated bistable snap-through peaks
FIG. 10 — stress-strain data from Instron testing: each peak is one bistable snap-through
PROJECT SHEET 3 OF 4 — ZONE C2

HAB / NEBP

FLOWN

Two years with the National Eclipse Ballooning Program (NEBP), coordinating a team of eight across five high-altitude balloon launches. Payloads reached the edge of space, past 100,000 ft, on multiple flights, and instrumentation from one launch contributed to research on atmospheric gravity waves during a solar eclipse — work presented at the American Astronomical Society conference.

I designed the payload housings in SolidWorks and built them from foam-core panels, then built and programmed the ozone sensor module in C++ for onboard readout and logging. Each payload carried an Iridium satellite modem and GPS for tracking, recovered afterward with a portable ground station and directional antenna. I also helped coordinate launch-day logistics and team roles across the five missions.

Max altitude100,000+ ft
Launches5
Team size8
FirmwareC++
TelemetryIridium + GPS
PresentedAAS Conference
ROLE — Designed payload housings in SolidWorks · built & programmed the ozone sensor module (C++) · operated ground tracking station · coordinated a team of 8 across 5 launches
Balloon ascending with a string of orange payload boxes
FIG. 1 — payload train climbing on tow, six housings on lines below the balloon
3D visualization of the balloon flight path over the White Mountains
FIG. 2 — reconstructed flight path over the White Mountains, near Mt Moosilauke
Onboard camera view of Earth's curvature near the edge of space
FIG. 3 — onboard cameras, near apogee
SolidWorks model of the payload housing
FIG. 4 — payload housing, modeled in SolidWorks
Team assembling foam-core payload boxes in the shop
FIG. 5 — assembling foam-core housings pre-launch
Team operating a directional tracking antenna and ground station
FIG. 6 — ground station, tracking descent live
Onboard avionics with Iridium modem and flight computer
FIG. 7 — avionics bay: Iridium modem, GPS, flight computer
Payload parachute caught in a tree during recovery
FIG. 8 — recovery day, payload snagged high in the canopy
PROJECT SHEET 4 OF 4 — ZONE C3

RENU Turbine

COMPETED

With Renewable Energy at Northeastern (RENU), I designed the blade pitch-control mechanism for a three-person team's entry in a collegiate competition wind turbine build. Instead of a fixed blade angle, each blade mounts to a rotating shaft through a bearing housing, so pitch can be actively adjusted to the wind rather than staying fixed across every condition.

I modeled the full pitch assembly in SolidWorks — the bearing housing, mounting bracket, shaft, and hub — sized so the blade could rotate freely under load without binding. Active pitch control measured roughly an 8% efficiency gain over a fixed-blade baseline across varying wind speeds.

Efficiency gain~8%
Team size3
Competition rank6 of 10
MechanismActive pitch
CADSolidWorks
Fabrication3D print + shop
ROLE — Designed & modeled the blade pitch mechanism (bearing housing, bracket, shaft, hub) in SolidWorks · contributed to the team's competition build
CAD assembly of the blade pitch mechanism, shaft, and bearing housing
FIG. 1 — full pitch assembly: blade, mounting bracket, bearing housing, shaft
Close-up of the blade mounted to the pitch bracket
FIG. 2 — blade mounted to the pitch bracket, free to rotate on the shaft
CAD model of the turbine hub with internal mechanism
FIG. 3 — hub, modeled with internal clearance for the pitch linkage
REVISION HISTORY

Timeline

IN PROGRESS
RevDateDescription
A2016–2025Boy Scouts of America — Senior Patrol Leader (3 yrs), 300+ community service hours, Welding Merit Badge, Eagle Scout
B2021–2025Hanover High School — Crew Team Captain, Environmental Club President; Shift Lead, Hanover Brick & Brew Restaurant
C2021–2023National Eclipse Ballooning Program — coordinated a team of 8 across 5 launches to 100,000+ ft
D2025Enrolled at Northeastern University — B.S. Mechanical Engineering, Aerospace Engineering minor
E2025Joined Alpha Kappa Sigma (AKS) Fraternity; began volunteering with the Lyme Fire Department
FFall 2025Dean's List
GDec 2025Began undergraduate research, Transformative Robotics Lab, under Prof. Jeffrey Lipton
CURRENT2026BETR cylinder characterization (TRL) · pitch-control system for RENU's competition wind turbine · CSWA certification in progress
TITLE BLOCK — FINAL SHEET

Contact

OPEN TO INTERNSHIPS / CO-OP
LocationBoston, MA / Hanover, NH
ProgramB.S. ME, Northeastern '29
Reach out about mechanical engineering or robotics internships and co-ops, research collaborations, or just to talk about bistable structures and things that fly higher than they should.