Tufts CubeSat Team

Building Tufts's first satellite to see space debris before it becomes a threat.

SPACE RACCOON is a 2U CubeSat mission using onboard computer vision and machine learning to detect, classify, and assess collision risk in Low Earth Orbit.

CubeSat form factor
2U
CubeSat form factor
Low Earth Orbit
LEO
Low Earth Orbit
Mission duration
14 mo
Mission duration
Target launch
2029
Target launch
SPACE RACCOON CubeSat CAD model with exploded internal stack

The mission

From launch pad to open data.

01 / 07 · Target 2029

Launch

After two to three years of design and testing on campus, SPACE RACCOON rides to orbit as a compact 2U CubeSat: the first satellite ever built at Tufts.

  • 2U CubeSat
  • COTS components
  • Systems engineering

02 / 07 · Low Earth Orbit · 14 months

Reach orbit

Deployed into Low Earth Orbit for a 14-month mission, the satellite runs on body-mounted solar cells and holds its attitude with in-house reaction wheels.

  • Electrical power system
  • ADCS
  • Reaction wheels

03 / 07 · Vision payload

Detect

During scheduled imaging windows a modified GoPro captures a frame every 30 seconds, searching for debris against the star field.

  • GoPro payload
  • Imaging windows
  • Onshape CAD

04 / 07 · Onboard computer vision

Classify

Image processing isolates each object and a neural network classifies it (fragment, rocket body, defunct satellite) right on the spacecraft.

  • Python → C image processing
  • Neural network
  • FPGA
  • Flight software

05 / 07 · Collision screening

Assess the risk

Tracks across frames feed a collision-risk assessment that flags the objects that matter most to anything else flying in LEO.

  • Orbital mechanics
  • Linear algebra
  • Risk scoring

06 / 07 · VHF / UHF

Downlink

Only frames that contain debris are compressed, packetized, and sent over our radio link to a student-built ground station.

  • Transceiver & antenna
  • Link budget
  • Ground station
  • Packetization

07 / 07 · Open source

Open to everyone

Flight software and debris data are released openly to support safer orbital operations and the student teams that come after us.

  • Open-source software
  • Open data
  • GitHub
FRAGMENT 0.94DEFUNCT SAT 0.88ROCKET BODY 0.81FRAGMENT 0.76COLLISION RISKHIGH · DEFUNCT SAT</> OPEN DATA

Inside SPACE RACCOON

Every layer, built by students.

A 2U CubeSat is just 10 × 10 × 22.7 cm. Inside that volume each subteam owns a slice of the stack: the chassis and orbit analysis, power, flight software and vision, and the radio link home.

  • Structures
  • Software
  • Power
  • Comms
Antenna deckCOMMSVHF/UHF transceiverCOMMSPower system & batteryPOWERADCS · reaction wheelsSOFTWARE · STRUCTURESFlight computer & FPGASOFTWAREGoPro vision payloadPAYLOAD · SOFTWARE2U aluminum chassisSTRUCTURESSolar panelsPOWER

Roadmap

This year on the way to launch.

Full timeline →
  1. September

    • Avionics board complete
  2. October

    • Image processing software complete
    • Avionics board tested
  3. November

    • Structure design prototype manufactured
  4. December

    • ADCS board design complete
  5. February

    • Flight software complete
    • Reaction wheel manufacturing complete
  6. March

    • More to come…

Where we and our alumni work

Skills from CubeSat carry into industry. We also collaborate with MIT and UMass Lowell.

  • Medtronic
  • Draper
  • NVIDIA
  • Blue Origin
  • Takeda
  • MITRE
  • Amazon Robotics
EmailWilliam.Goldman@tufts.edu
LocationHalligan Hall, Tufts University
GitHubTufts-CubeSat

Last updated: September 27, 2026