PROJECT ARCHIVE

BUILT.
TESTED. FLOWN.

A record of Endeavour’s evolving vehicles, engines, aircraft, test systems and research programmes.

2026—27

CURRENT
TRAJECTORY

Galvan leads the sounding-rocket programme. Payload combines payload science and spacecraft development, alongside a consolidated R&D team.
01

Project Galvan

Sounding Rocket

Endeavour’s first competition-scale SRAD liquid rocket.

A unified vehicle programme bringing aero-propulsion, recovery, avionics, software and payload together for the 30,000 ft liquid category at IREC 2027.

IREC 202730,000 ft · Liquid~35 members
Payload project hardware02

Project Aetherial

Payload

Endeavour’s payload team, from atmospheric instruments to compact spacecraft.

The team unites flight science and spacecraft development through experiments, the iSpex-derived spectropolarimeter and a modular PocketQube platform for remote sensing and future flight heritage.

SpectropolarimetryPocketQubeFlight science
03

Advanced concepts

Research & Development

One team for Endeavour’s most experimental technologies.

Dynamis, B-Star, XENITH and Fingal now sit within R&D, covering throttleable propulsion, active control, electric propulsion and landing demonstrators.

DynamisB-StarXENITH · Fingal
04

Education

Outreach

Hands-on rocketry for schools and communities.

Workshops, UKROC mentoring and public activities delivered with technical-team support to make aerospace accessible to every age group.

4 UKROC teamsAll reached regionalsAges 2–70

2025–26

SYSTEMS IN MOTION

Competition flight, propulsion, ground systems and active control matured in parallel.
Splinter project hardware01

Competition rocketry

Splinter

Launch 4 Change winner with a supersonic climate-science mission.

Shredder reached 4.2 km and Mach 1.16 on an L1115 motor, streamed live telemetry and video, and returned the launch vehicle in perfect condition. Its independently deployed spectropolarimeter payload measured the optical properties needed to build vertical aerosol profiles.

1st at L4C4.2 kmMach 1.16
02

Liquid propulsion · TVC

Gadget

Gizmo engine development paired with the Widget thrust-vector-control platform.

The team developed a 2 kN regeneratively cooled engine and a gimballed thrust plate, supported by design reviews, purchasing records and regular technical meetings.

2 kN targetRegenerative coolingThrust vectoring
03

Flight propulsion

Pegasus

A flight-ready liquid propulsion stack and the Cerberus multi-chamber engine.

Pegasus worked on tanks, feed systems, ignition, ablative chambers and a three-chamber Race 2 Space engine concept targeting roughly 6 kN total thrust.

Cerberus~6 kN targetRace 2 Space
04

Ground systems

Selidor

A staged liquid-engine test stand and operations programme.

Selidor integrated structure, fluid panels, purge, control, wiring and data acquisition to create Endeavour’s pathway toward independent hotfire testing.

DAQFluid systemsHotfire operations
05

Active control

A-StaR

Repeatable training rockets for avionics, simulation and active-stabilisation work.

A-StaR succeeded Bayes with small launch vehicles, flight computers, PID canards, grid fins and a stronger emphasis on regular testing and member training.

PID controlGrid finsTraining launches

2019–25

FOUNDATIONS IN FLIGHT

Projects developed between 2019 and 2025 established much of Endeavour’s present technical heritage.
01

Competition rocketry

Darwin

ADA-II and the ASIMOV test programme developed recovery, avionics, structures and payloads.

Darwin’s approximately 30 members used smaller rockets to test systems before integrating a 3 km competition mission with dual deployment and a deployable rover payload.

ADA-II3 km mission~30 members
02

Liquid propulsion

Maxwell

The society’s bipropellant engine team and predecessor to later propulsion programmes.

After WeeMaxwell achieved a 26-second hotfire, Maxwell pursued a 2.5 kN nitrous oxide and isopropyl alcohol engine, piston tanks and an integrated test system.

26 s hotfire2.5 kN targetBest Biprop
03

Uncrewed aircraft

Rankine

A fixed-wing autonomous aircraft for the IMechE UAS Challenge.

A 36-member multidisciplinary team developed a payload-focused aircraft with avionics, simulations, ground systems and a formal concept-to-flight review process.

36 members3.36 kg payload20 km design range
04

Active control

Bayes

Endeavour’s early active-flight-control and onboard data programme.

Bayes flew a datalogger on Starscout to roughly 750 m, recovering orientation and altitude data while exploring actively controlled test vehicles.

~750 m flightFlight dataloggerActive control