

A CubeSat constellation for atmospheric analysis of Earth
Mission objectives
CHESS is a Swiss space initiative federating academia and industry partners to drive multiple space experiments through the development of Swiss-made scientific instruments. The main science objective is to improve the understanding of the upper atmospheres of planets by in-situ measurements.
Taking advantage of the popular, cost-effective CubeSat standard, we hereby propose a constellation of identical nanosatellites to study the composition of the terrestrial atmosphere and its density.

Mission Profile
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Constellation of 2x 3U Cubesats
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Launch on a Low Earth Orbit with one circular orbit and one elliptical
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Flight time of 2 years (min.)
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Launch target: Q4-2022
Scientific objectives
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Measure Earth’s present chemical composition, and its evolution over time.
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Understand the variation of the composition of the exosphere. The time scales and the driving mechanisms
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Proof that this low-cost and miniaturized measurement technology has a major impact on our understanding of planetary atmospheres to pave the way for installing similar probes into extraterrestrial atmospheres

Main payload
The latest valuable scientific data of Earth’s exosphere composition with a mass spectrometer was recorded back in 1983 and performed with now-outdated technology, with modest sensitivity thus leading to poor-quality isotope patterns. UniBe, therefore, invented a state-of-the-art, 10-cm-class, low-cost time-of-flight mass spectrometer, the CubeSatTOF, which fits into 1U of a CubeSat. CubeSatTOF features outstanding performance for its size, offering a sensitivity rate and a dynamic range comparable to NIM/PEP/JUICE - a 30-cm-class instrument also developed by the University of Bern.
Developed by UniBern Size: 1U (10x10x10 cm)
Mass: 1 kg Power consumption: 7 W


Secondary payloads
CHESS offers a unique framework for Swiss research institute or industry to validate new technology or scientific instrument. Our CubeSat platform is designed to embark on multiple, small, secondary payloads. Among them, we have a next-generation GNSS, a new type of solar cells, and a radio amateur payload allowing us to use their frequency bands.
Our 3U CubeSat platform


Our vision:
Use simple, flight-proven subsystems and perform exhaustive testing to minimize the risk of mission failure
In-house built subsystems:
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On-Board Computer by HES-SO
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X-band transmitter, by HSLU
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UHF/VHF transceiver by HSLU
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GNSS, by ETHZ
COTS subsystems:
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ADCS, with reaction wheels
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EPS: power distribution board, battery, solar panels
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Structure
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X band and UHF-VHF antennas

Les différents acteurs
Organization

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Information session
Monday, 18th at 18:00 I On Zoom
All information you need if you want to join the Team!