Ethan Sheehan

Ethan Sheehan — Aerospace engineering at the University of Bristol. Propulsion Lead, HyPower Bristol.

Aerospace engineering at the University of Bristol Bristol, UK

Engine 1, Test 3 at steady state on the Airborne Engineering thrust stand

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Test footage 16 clips — 7 programmes

I build and fire liquid rocket engines.

MEng Aerospace Engineering student at the University of Bristol and Propulsion Lead at HyPower Bristol. Three research internships alongside it: the Bristol Flight Lab and the Bristol Composites Institute in 2025, ILK Dresden in 2026.

Three years on BristolSEDS Experimental Propulsion, Engine Lead then Propulsion Lead across four engine programmes, including the 5.94 kN regeneratively-cooled engine that set the UK student thrust record in January 2025.

5.94 kN
UK student thrust record, Jan 2025
4
liquid engine programmes led
>80,000 N·s
total impulse fired
18
test firings, engines and igniters
BSEP Engine 1 — Maleficent

Ignition, slow motion. The plume establishing on Test 3.

01 — Propulsion: BSEP

Four engines, a torch igniter, and the fires that proved them.

FIVE
Test 1 hot fire from the AEL cell camera: ignition, a 3 s burn and shutdown
01 — Engine Lead — 2024-25

BSEP Engine 1Maleficent

Regeneratively-cooled Inconel 718 bipropellant engine. 5.94 kN in January 2025: the UK student thrust record.

Peak thrust
5.94 kN
Chamber pressure
23.55 bar
Hot fires
6
Full case study →
Cell camera view of the burn: a yellow ignition plume turns purple, then a fireball, then the engine shuts down
02 — Propulsion Lead — 2025

BSEP Engine 2Snow White

The world's first CP1 aluminium rocket engine: a lightweight Al-Fe-Zr chamber with a coaxial-swirl injector, run to full duration on its maiden fire.

Peak thrust
2.1 kN
Burn
5.0 s full duration
Chamber mass
~3x lighter
Full case study →
Interactive 3D model of the Engine 3 chamber with the outer wall left off, so the helical regenerative cooling channels wrapping the chamber and throat are the visible surface. Drag to orbit.

Loading model 0%

03 — Propulsion Lead — 2025-26

BSEP Engine 3Rapunzel

Spiral-channel regen chamber built for flight: designed, printed in CP1 aluminium and CT-scanned end to end, waiting on its first hot fire.

Design thrust
5 kN
Channels
56 spiral
Peak wall temp
664 → 632 K
Full case study →
Interactive 3D model of Engine 4: a chamber wrapped in a diamond isogrid lattice, a bolted injector flange at one end, a nozzle at the other, and one of the L-brackets it mounts on. Drag to orbit.

Loading model 0%

04 — Propulsion Lead — 2025-26

BSEP Engine 4Elsa

Bristol's first LOx/IPA engine, for Race 2 Space 2026.

Design thrust
5 kN
Burn
8 s
Oxidiser
LOx
Full case study →
Close GoPro clip of the final burn: the igniter runs for several seconds, then flame breaks out of the body wall and a shower of sparks erupts.
05 — Propulsion Lead — 2024-25

BSEP Torch IgniterTuppence

Hydrogen/oxygen torch igniter: eight firings, retired after melting through 5 mm of stainless.

Firings
8
Inlet pressure
3→12 bar
Wall
5 mm melted through
Full case study →
02 — Flight campaigns: HyPower

Taking the engines to the stand and to Portugal.

TWO
Wide 4K view of the test bay from outside: the sparkler ignites in a shower of sparks, a short orange plume streams out of the bay, then white vapour as the oxidiser runs out
06 — Propulsion Lead — September 2025

Integrated Test Campaign 2025

Engine and feed-system flight qualification for EuRoC 2025: three burns in September, a 7 s full-duration firing and a 5.58 kN peak on the last.

Burns
3
Full-duration burn
7 s
Peak thrust
5.58 kN
Full case study →
Handheld pan along the flight propulsion system on the bench: the printed chamber and bell nozzle, the injector and valve block with its feed lines and pressure transducers, then the white tank sections and their bulkhead plumbing
07 — Propulsion Lead — 2025

EuRoC 2025Waxwing

HyPower's 2025 vehicle at the European Rocketry Challenge: 25 teams, first of the UK entrants, grounded 800 m from the pad.

Teams
25
UK entrants
1st
Vehicle
83 kg, 4 m
Full case study →
03

Control systems.

TWO
Bench telemetry for the 7 bar test: supply pressure decaying from 15.9 to 10.4 bar, regulated pressure rising to about 6.5 bar against the 7 bar setpoint, and the servo transient
08 — Propulsion Lead — 2026

BSEP E-Reg

An electronic pressure regulator for HyPower's pressure-fed rockets: a servo ball valve and a gain-scheduled cascade PID on an STM32, simulated, verified bit-exact into flight C, then bench-tested.

Design point
300 → 55 bar
Bench tests
8
Sim → flight code
Bit-exact
Full case study →
Descent and landing of Monte-Carlo run 59: altitude above ground against crossrange, the vehicle drawn at its own logged attitude every few seconds with the plume shown where thrust is commanded, flaring to touchdown 660 m downrange
09 — Year-3 individual research project — 2025-26

Landing a TVC Rocket After Main Chute Deployment

Landing a thrust-vector-controlled sounding rocket after main-chute deployment: a 3-DOF Simulink simulation, a phased LQR controller and a 300-run Monte-Carlo campaign.

Monte-Carlo success
70%
Best landing pitch
−0.63°
Engagement altitude
200 m
Full case study →
04

Machine learning development and research.

FOUR
Third-person Unreal chase view of the minidrone rounding the corner of the red L-track above a grey arena floor with yellow and blue decoy squares
10 — MathWorks Minidrone Competition — 2026

Optimal Line-Following DroneBOLD

A reinforcement-learning path planner for the MathWorks Minidrone Competition Europe 2026: a Parrot Mambo follows a red line and lands on the marker, with the policy shipped as baked weights and zero toolbox dependency.

Held-out tracks
40 / 40
Cross-track RMS
43.8 mm
Benchmark policy
46.2 mm
Full case study →
Live dashboard frame: a hand-held specimen with the fine-stage crop box and detected tip drawn in the stream
11 — Research intern — 2026

ILK DresdenTorchCrack

Live AI crack-tip detection for composite fracture tests, running on a Jetson AGX Orin. Summer 2026.

Live rate
~25 fps
Frame
5 MP
Compute
1 Jetson
Full case study →
Pan across the tensile rig during a live test, from the Shimadzu frame to the acquisition monitor
12 — Research intern — 2025

Bristol Composites Institute

Curvature-to-stress prediction for 3D-printed flax/PLA hygromorph strips: 72 specimens, 10 batches, and a paper on why the shape transfers and the scale does not.

Master-curve R²
0.92
Specimens
72 / 10 batches
Self-calibration R²
0.74
Full case study →
Eighteen-by-eighteen head-to-head matrix from the agent tournament: every pair of agents decided by SPRT, each cell a win percentage carrying its own sample count, green where the row agent wins and red where it loses.
13 — Environment and evidence, two-person team — 2026

Pokémon TCG Agent

Kaggle Pokémon TCG AI Battle, summer 2026. The agent was three behaviour-cloned networks and a shallow search; the product was the measurement instrument that reversed six of our own decisions before they shipped.

Games per arm
140,000
Sampled gain
+7.48 pp
Argmax gain
+0.20 pp
Full case study →
05 — Other projects

CFD validation, and a toolchain the Flight Lab still runs.

TWO
The ARIA nose swept as a body of revolution with the computed wall pressure coefficient painted on its surface: compression warm at the tip, falling through zero along the nose, a strong expansion band at the shoulder, then recovery along the afterbody. Drag to orbit it, hover to read the station.
14 — Propulsion Lead — 2026

Nosecone CFDARIA V&V

Density-based OpenFOAM simulation of the ARIA sounding-rocket nosecone at Mach 1.8, validated against NACA wind-tunnel data to within the tunnel's own uncertainty.

Mean |ΔCp| vs wind tunnel
0.0040
Apex p/p∞ vs exact theory
+0.2 %
LTS speed-up
12.7×
Full case study →
The AVDASI 2 docs landing page in July 2025: Flight Lab red header, a paragraph explaining the auto-synced code repo, and Avionics, Aerodynamics and Structures sections in the left nav
15 — Intern — Summer 2025

Bristol Flight Lab

AVDASI2 avionics teaching resources: the Cube guide, an example ground station and the docs site the Flight Lab still runs.

Docs site
9 pages
Kept and extended
82 staff commits
In use since
July 2025
Full case study →
06 — Coursework

Assessed work, years one to three.

SEVEN
The finished BlueBird UAV on a bench trolley in the lab: full blue film-covered wing across two benches, silver instrument pod under the carbon fuselage spar, students in maroon lab coats working around it
16 — Avionics test lead, group design project — 2024-25

AVDASI 2: BlueBird AvionicsBlueBird

Avionics test lead on a six-person team: Hall-effect flap sensing, servo calibration, aircraft integration and three days in the wind tunnel.

Flap angle accuracy
1 deg bench, 1-3 deg tunnel
Tunnel campaign
3 days at 20 m/s
Servo calibration
3-stage
Full case study →
Integrated Test Campaign 2025

Hotfire 2, the full-duration burn. Shock diamonds hold the length of the plume.

Index

All 22 projects, filtered by topic.

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About

Ethan Sheehan

Bristol
Ethan Sheehan

MEng Aerospace Engineering student at the University of Bristol and Propulsion Lead at HyPower Bristol. Three research internships alongside it: the Bristol Flight Lab and the Bristol Composites Institute in 2025, ILK Dresden in 2026.

Three years on BristolSEDS Experimental Propulsion, Engine Lead then Propulsion Lead across four engine programmes, including the 5.94 kN regeneratively-cooled engine that set the UK student thrust record in January 2025.

DegreeMEng Aerospace Engineering, First class
InstitutionUniversity of Bristol
Dates2023-2027
PrizeRoderick Collar Prize
BeforeA levels: Maths, Further Maths, Chemistry, Physics. British International School of New York, 2021-2023
NowMEng year 4 at Bristol, Propulsion Lead at HyPower