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Project Stratosphere: Sustainable CubeSat Design & Simulation

Learn about the design of a low-cost 1U CubeSat for ozone layer monitoring. Features sensor selection, electronics simulation, and budget management.

#cubesat#stem-education#environmental-monitoring#satellite-design#arduino#atmospheric-science#aerospace-engineering
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EESW STEM CYMRU · 2025–2026
PROJECT
STRATOSPHERE
Design & Simulation of a Sustainable CubeSat for Ozone Layer and Atmospheric Monitoring Research over Wales
Gower College Swansea · University of South Wales
Lewis Whitefoot
Oleksandra Roshchupkina
Mahiba Hossain
Rayan Haque
Miles Li
Oliwier Lesiak
Made byBobr AI
01 / OVERVIEW
EXECUTIVE SUMMARY
Students at Gower College Swansea designed and simulated a functional, integrated 1U CubeSat prototype — cost-effective, sustainable, and scientifically rigorous — in response to a mission brief from the University of South Wales.
MISSION
Environmental monitoring — ozone layer & UV radiation research above Wales
BUDGET
£88.30 of £200 limit — 56% savings achieved
FORMAT
1U CubeSat · 10×10×10 cm · 1–3 kg · High-altitude balloon launch
MISSION AT A GLANCE
£88.30
Final Budget
10–20 km
Target Altitude
−50°C
Min. Temperature
2–8 ppm
Ozone Target Range
Ozone sensor (DFRobot Gravity, 0–10ppm)
Seeeduino Lotus Cortex M0+
EPP foam + Mylar thermal protection
LiPo battery cold-rated
Grove sensor ecosystem
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02 / MISSION DEFINITION
PROJECT STRATOSPHERE

MISSION AIM & OBJECTIVES

To design, simulate, and plan a low-cost high-altitude CubeSat payload gathering atmospheric data to support research into greenhouse gas effects on the ozone layer above Wales.

MISSION OBJECTIVES
01
Design complete sensing payload within £200 budget
02
Select ozone, UV, temperature, pressure sensors
03
Simulate electronics in Tinkercad
04
Calculate power consumption for −50°C operation
05
Design lightweight thermally insulated 10×10×10cm structure
06
Conduct full risk assessment & feasibility study
KEY PARAMETERS
Altitude Range
10–20 km
Temperature Range
−40°C to −50°C
Payload Format
1U CubeSat (10×10×10 cm)
Mass Limit
1–3 kg
Budget Cap
£200
Flight Duration
1.5–3 hours
Primary Target
Ozone Layer (15–35 km)
ENVIRONMENTALLY FOCUSED MISSION
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03 / SYSTEM DESIGN
SENSORS & ELECTRONICS
PAYLOAD COMPONENTS
SEEEDUINO LOTUS CORTEX M0+
01
12 Grove connectors · Arduino-compatible pins · LiPo battery support · ATSAMD21 chip
BRAIN / CENTRAL HUB
DFROBOT GRAVITY IIC OZONE
02
Range: 0–10 ppm · Resolution: 10 ppb · Electrochemical · £43.08
PRIMARY SCIENCE INSTRUMENT
GROVE GPS (AIR530)
03
50,000m altitude mode · No COCOM limit · Dual altitude verification · £11.77
TRACKING & RECOVERY
GROVE AHT20 I2C
04
Industrial grade · −40°C rated · I2C interface · £3.38
ENVIRONMENTAL MONITOR
GROVE BAROMETER SPA06-003
05
Primary altitude calc · Barometric formula · In Grove kit · £0.00
ALTITUDE REFERENCE
LIPO BATTERY 3.7V 2Ah
06
Cold-rated · Chemical heat packs added · EPP foam insulated · £22.10
POWER SUBSYSTEM
COMPONENT TOTAL: £88.30 / £200 BUDGET
56% BUDGET REMAINING
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Project Stratosphere: Sustainable CubeSat Design & Simulation

Learn about the design of a low-cost 1U CubeSat for ozone layer monitoring. Features sensor selection, electronics simulation, and budget management.

EESW STEM CYMRU · 2025–2026

PROJECT

STRATOSPHERE

Design & Simulation of a Sustainable CubeSat for Ozone Layer and Atmospheric Monitoring Research over Wales

Gower College Swansea · University of South Wales

Lewis Whitefoot

Mahiba Hossain

Miles Li

Oleksandra Roshchupkina

Rayan Haque

Oliwier Lesiak

01 / OVERVIEW

EXECUTIVE SUMMARY

Students at Gower College Swansea designed and simulated a functional, integrated 1U CubeSat prototype — cost-effective, sustainable, and scientifically rigorous — in response to a mission brief from the University of South Wales.

MISSION

Environmental monitoring — ozone layer & UV radiation research above Wales

BUDGET

£88.30 of £200 limit — 56% savings achieved

FORMAT

1U CubeSat · 10×10×10 cm · 1–3 kg · High-altitude balloon launch

MISSION AT A GLANCE

£88.30

Final Budget

10–20 km

Target Altitude

−50°C

Min. Temperature

2–8 ppm

Ozone Target Range

Ozone sensor (DFRobot Gravity, 0–10ppm)

Seeeduino Lotus Cortex M0+

EPP foam + Mylar thermal protection

LiPo battery cold-rated

Grove sensor ecosystem

02 / MISSION DEFINITION

PROJECT STRATOSPHERE

MISSION AIM & OBJECTIVES

To design, simulate, and plan a low-cost high-altitude CubeSat payload gathering atmospheric data to support research into greenhouse gas effects on the ozone layer above Wales.

MISSION OBJECTIVES

Design complete sensing payload within £200 budget

Select ozone, UV, temperature, pressure sensors

Simulate electronics in Tinkercad

Calculate power consumption for −50°C operation

Design lightweight thermally insulated 10×10×10cm structure

Conduct full risk assessment & feasibility study

KEY PARAMETERS

10–20 km

−40°C to −50°C

1U CubeSat (10×10×10 cm)

1–3 kg

£200

1.5–3 hours

Ozone Layer (15–35 km)

ENVIRONMENTALLY FOCUSED MISSION

03 / SYSTEM DESIGN

SENSORS & ELECTRONICS

PAYLOAD COMPONENTS

SEEEDUINO LOTUS CORTEX M0+

12 Grove connectors · Arduino-compatible pins · LiPo battery support · ATSAMD21 chip

BRAIN / CENTRAL HUB

DFROBOT GRAVITY IIC OZONE

Range: 0–10 ppm · Resolution: 10 ppb · Electrochemical · £43.08

PRIMARY SCIENCE INSTRUMENT

GROVE GPS (AIR530)

50,000m altitude mode · No COCOM limit · Dual altitude verification · £11.77

TRACKING & RECOVERY

GROVE AHT20 I2C

Industrial grade · −40°C rated · I2C interface · £3.38

ENVIRONMENTAL MONITOR

GROVE BAROMETER SPA06-003

Primary altitude calc · Barometric formula · In Grove kit · £0.00

ALTITUDE REFERENCE

LIPO BATTERY 3.7V 2Ah

Cold-rated · Chemical heat packs added · EPP foam insulated · £22.10

POWER SUBSYSTEM

COMPONENT TOTAL: £88.30 / £200 BUDGET

56% BUDGET REMAINING

  • cubesat
  • stem-education
  • environmental-monitoring
  • satellite-design
  • arduino
  • atmospheric-science
  • aerospace-engineering