Portfolio / Mechanical & Aerospace Engineering

Wallace Tucker

Mechanical engineer at Colorado State, specializing in rotorcraft systems and aerodynamics.

Undergraduate capstoneHexacopterCustom-designed, modular and packable, 1,250 mm wheelbase
Graduate capstoneRotor designOptimized for variable pitch, ~0.8 figure of merit predicted
Rowing1stHead of the Charles 2025, collegiate age group
Rowing5th of 32ACRA national championships, men's double, 2025
See how the hexacopter is built
DegreeM.S. Mechanical Engineering
SchoolColorado State University
GraduatingSpring 2027
Thesis focusRotor blade design, figure of merit
Wallace holding the hexacopter with all six arms extended in an open field
The medium-lift hexacopter at full 1,250 mm wheelbase.

Thesis

In progress

My master's research is on rotor blade design and aerodynamic optimization, with figure of merit as the main measure of hover efficiency. The idea is one aircraft, several blades: instead of compromising on a single blade, I design a family of blades for the same airframe and match the blade to the mission. The blades are optimized for variable-pitch operation.

Endurance blade

Long loiter and survey. Lightly loaded with a slower tip speed, tuned to spend the flight at its most efficient. Predicted figure of merit is about 0.8 in simulation.

Utility blade

Heavy lift and high power. More blade area and a higher tip speed for payloads and hot, high days, designed for about 5,500 ft elevation.

What figure of merit means in watts

Figure of merit is hover efficiency: the power an ideal rotor would need to lift a weight, divided by what the real rotor needs. 1.0 is perfect, and good rotors are near 0.8. Move the sliders to see how much power a better blade saves.

Figure of merit 0.50, a poor blade-
Figure of merit 0.65-
Figure of merit 0.80, a well-designed blade-

Hover power at 5,500 ft (air density 1.036 kg/m3), single rotor. Simple momentum theory; real aircraft add motor and transmission losses.

Against the props on the hexacopter

The same question on real hardware. The measured curve is bench data for the 22 in props currently on the hexacopter. The dashed line is what a 0.80 figure of merit rotor of the same diameter would draw on the same motor and ESC.

-Current props, per rotor
-0.80 FoM rotor, per rotor
-Less power, same thrust
Current props (measured)0.80 FoM rotor (estimated)
Show the data as a table
Thrust gfPower Wgf/W0.80 FoM Wgf/W

Assumptions: 22 in rotor, air density 1.036 kg/m3 (5,500 ft). I treat the table's power as electrical input, so the 0.80 rotor's shaft power is divided by an assumed 85% motor and ESC efficiency. The 0.80 figure is simulated for my larger-scale blades; at 22 in lower Reynolds numbers will give back some of it. Bench data covers 0.5 to 4.0 kgf per rotor.

Manufacturing and fabrication

Design for manufacture

I design parts knowing how they will be made. Since Fall 2023 at the Rapid Prototyping Lab I have taken parts from CAD through printing, casting, machining and assembly, and chosen the process that fits each one.

FDM printing

Bambu Lab, Creality, Snapmaker, Prusa, MakerBot and Markforged, from quick prototypes to functional parts.

SLA resin printing

Clear valve cover for a working model engine, so the valves and combustion LED show through.

SLS part design

Designed SLS versions of drone parts for a research project in an advanced additive manufacturing course.

Silicone casting

Silicone bumpers bonded to aluminum for pneumatic gripping.

Composites

Wet layup glass over foam core, and prepreg skins. Both used on a tested composite beam.

Design around stock

Structures built around prefab composite tube and plate, so parts are cut, bonded and machined instead of molded.

CNC milling

3-, 4- and 5-axis work on Haas mills, programmed in Fusion CAM.

CNC turning

Haas CNC lathe, programmed in Fusion CAM.

Laser, waterjet and sheet metal

CO2, fiber and diode lasers. A 3-axis Flow waterjet with BobCAD and Fusion CAM. Sheet metal bending.

Electronics fabrication

PCB design in KiCad, with surface-mount reflow and through-hole assembly.

Projects

Selected work

Aerospace and UAV

Featured / Undergraduate capstone

Medium-lift hexacopter

Modular, packable electric hexacopter with a 1,250 mm wheelbase. All six arms come off and pack into a single rifle case, ready to fly in under 3 minutes.

1,250 mmWheelbase, motor to motor
10 kgAircraft
1 to 10 kgDesign payload
< 3 minCase to flight
40 minUnloaded, lithium-ion pack
9 kgThrust per motor

Capstone team: Medium Lift Hexacopter. I designed the core, arms, landing gear and motor mounts, manufactured most of the parts, and handled the ArduPilot work. Teammates handled payloads and regulatory work.

The hexacopter on the ground at dusk with its motor-mount lights lit
Ground check at sunset with the motor-mount lights on.
Removable arms

Each 450 mm arm releases from the core and carries a MAD M6C10 EEE 300 KV motor with a 22 x 7 folding polymer prop. Power and signal connect through blind-mate blade connectors on fully custom boards, as the arm seats mechanically, so there are no hand-plugged connectors. Arms are built around prefab carbon tube and held by grade 5 titanium cam levers. LED lighting boards are mounted on each motor mount. About 25 attach and detach cycles so far, without incident.

Motor mount with integrated ESC

The TBS Lucid AM32 ESC is built into the motor mount, with CFD-optimized, five-axis-machined heat sinks and cooling fins. Each mount runs 60 A at 6S. Thrust is about 9 kg per motor at sea level and 8 kg at 5,000 ft. In an 18-minute hover test, temperatures stayed at normal operating levels and no temperature warning was raised in flight.

The hexacopter hovering against a clear sky during the 18-minute test
Hovering during the 18-minute test.
Core structure

A custom isogrid hexagon machined from 6061 on five axes: 85 mm sides, 5 mm walls, 100 mm tall, under 300 g.

The isogrid core is more than 55% lighter than a plain tube and about 94% lighter than a solid block of the same size. Calculated for an 85 mm hexagon, 100 mm tall, in 6061 at 2.70 g/cm³.

The hexacopter core with red cam levers, carbon plates and tube arms
The core with arms clamped by titanium cam levers.
The core being machined on a five-axis mill under coolant
The core during machining.
Landing gear

Ladder-style legs made of carbon tubes bonded to carbon plates. Spring pins make them quick to swap.

Landing gear photos go here.
Battery pack

A 6S8P lithium-ion pack of EVE Energy 50PL 21700 cells (5000 mAh each, 40 Ah, about 864 Wh nominal) weighs 3.5 kg and reached 40 minutes unloaded, with a 350 A peak rating. The EVE 50PL won a four-cell shortlist on cost: at about $5 per cell, the 48 cells cost roughly $240, or about $280 per kWh. The original pack is 6S4P 5450 mAh LiPo cells built into a single unit, held together by carbon plates and secured with thumbscrews for quick swaps. It weighs 3.2 kg and flew 22 minutes unloaded with about 30% battery left.

The lithium-ion pack holds about 80% more energy for about 9% more weight. Energy figures use nominal cell voltages (3.6 V lithium-ion, 3.7 V LiPo).

Pack photos go here.
Flight controller and navigation

Cube Orange running ArduPilot, with a Here3 RTK GPS and a Mauch power module. I configured the waypoint missions and handled the ArduPilot work after initial setup.

Inside the hexacopter core: Cube Orange flight controller and wiring
Cube Orange and power wiring inside the core.
Graduate capstone

Rotor design and testing

Blade design and aerodynamic optimization for hover efficiency, optimized for variable pitch and tested on scaled rotors.

Scaled rotor design

Candidate blade layouts defined station by station, then scaled for bench testing.

A 3D-printed scaled rotor blade on a printer bed
Printed scaled blade for bench testing.
UAV

Custom aircraft

Multirotors designed and built from the frame up, in long-range, freestyle and tiny whoop classes.

Long-range 7 inch

Custom long-range build on 7 inch props and 1750 KV motors. It reaches 22 minutes of maximum flight time on custom li-ion batteries.

The custom 7 inch long-range quadcopter on a workbench
The 7 inch long-range build.
Freestyle 5 inch

A generatively designed 5 inch frame. It weighs 400 g all up and flies for 5 to 15 minutes.

The generatively designed 5 inch freestyle quadcopter with green props
The 5 inch freestyle build.
Tiny whoop

A 60 g build on a custom frame with 2 inch props.

The tiny whoop on a scale reading 59.3 grams
The tiny whoop on the scale at 59.3 g.

Manufacturing

Manufacturing

Model four-stroke engine

A working 4-cylinder, 4-stroke model engine, motor-driven, with LEDs that show combustion. I designed and made every part, and built the electronics that run it.

Design

Mechanical parts are aluminum and polymers. The frame is mostly acrylic, so every moving part is visible.

CAD and drawings go here.
Fabrication

I machined the rotating assembly, block and valvetrain on CNC machines. A clear SLA-printed valve cover shows the valves and the combustion indicator LED.

Machining and assembly photos go here.
Electronics and controls

I built the full electronic setup: LEDs that show combustion, an RPM indicator, and safety interlocks including an e-stop and a motor switch.

Wiring and control panel photos go here.
Running

It runs continuously on my shelf at about 42 rpm.

The model engine running in a dark room with its cylinders lit and a red combustion glow
Running in a dark room, with the combustion LEDs lit.
The engine running, with its RPM display.
Manufacturing

Composite beam

A foam-core beam with 10-ply prepreg skins, tested in three-point bending.

795 lbPeak load
179 gBeam mass
21 inBeam length
~2,000xLoad / own weight
Design

A 1.25 in foam core wrapped in wet-layup glass fiber, so it can withstand vacuum pressure.

Beam cross-section sketch goes here.
Fabrication

Prepreg top and bottom skins, 10 plies each: six at 0 degrees, two at +45 and two at -45.

A composite beam on a lab scale before its outer carbon skin
Weighed on the bench before the outer carbon skin.
Composite beam layup on a work table under vacuum film
Layup and cure.
Testing

Three-point bending. The beam carried a peak load of 795 lb at 21 in long and weighed 179 g.

The composite beam loaded in a three-point bending fixture on a materials testing machine
The beam under three-point bending.

Skills

Tools & processes
Fusion 360 and Fusion CAM8 yrs / high
SolidWorks4 yrs / high
KiCad (schematics and PCB layout)3 yrs / high

Electronics. PCB design and assembly, surface-mount (reflow) and through-hole.

Flight systems. ArduPilot setup, FPV and multirotor builds.

Analysis. QBlade (blade element momentum theory), MATLAB and CFD.

Experience

Colorado State University
Spring 2026 to present

Teaching Assistant, EMEC

Fall 2023 to present

Rapid Prototyping Lab

  • Led 3 to 4 projects, details under NDA, alongside many lab projects
  • CNC subtractive manufacturing
  • 3D modeling and design of complex systems
  • Additive manufacturing
  • PCB design and manufacture with SMD and THT components

Beyond engineering

Personal

Rowing

Competitive sculler for Colorado State Club Rowing, and its president for two years. ACRA is the American Collegiate Rowing Association, which runs the club national championships.

5th of 32ACRA national championships, men's double, 2025
10 → 30Club members, start to end of my term
2 → 15Nationals qualifiers, start to end of my term
  • First in the collegiate age group of the Men's Championship Double at the 2025 Head of the Charles.
  • Two 10th-place finishes in the open-weight men's single at the ACRA national championships, in fields of 19 and 34.
  • Many regional podiums and wins, and consistently the fastest single sculler in the region.
  • Club president for two years, membership and nationals qualifiers grew as shown above.
  • Travel safety lead for one year before becoming president: planned trips, hotels and rental cars, and owned on-water safety.
Wallace smiling with a gold medal between two teammates
On the podium.
Wallace racing a single scull on a river
On the water.
Wallace biting a gold medal in a Colorado State rowing uniform
After the race.

Hiking and mountaineering

Trail hiking and mountaineering.

Wallace in a climbing helmet resting on a mountain slope
Mountaineering.

Contact

Open to full-time roles