Change search
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf
Space Environmental Chamber for Planetary Studies
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology.ORCID iD: 0000-0003-0499-6370
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology.ORCID iD: 0000-0002-7148-8803
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology.ORCID iD: 0000-0003-2691-3855
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology. Centro de Astrobiología (CSIC-INTA), Torrejón de Ardoz, 28850 Madrid, Spain; School of Geosciences, University of Aberdeen, Aberdeen, AB24 3FX, UK.ORCID iD: 0000-0002-4492-9650
Show others and affiliations
2020 (English)In: Sensors, E-ISSN 1424-8220, Vol. 20, no 14, article id 3996Article in journal (Refereed) Published
Abstract [en]

We describe a versatile simulation chamber that operates under representative space conditions (pressures from < 10−5 mbar to ambient and temperatures from 163 to 423 K), the SpaceQ chamber. This chamber allows to test instrumentation, procedures, and materials and evaluate their performance when exposed to outgassing, thermal vacuum, low temperatures, baking, dry heat microbial reduction (DHMR) sterilization protocols, and water. The SpaceQ is a cubical stainless-steel chamber of 27,000 cm3 with a door of aluminum. The chamber has a table which can be cooled using liquid nitrogen. The chamber walls can be heated (for outgassing, thermal vacuum, or dry heat applications) using an outer jacket. The chamber walls include two viewports and 12 utility ports (KF, CF, and Swagelok connectors). It has sensors for temperature, relative humidity, and pressure, a UV–VIS–NIR spectrometer, a UV irradiation lamp that operates within the chamber as well as a stainless-steel syringe for water vapor injection, and USB, DB-25 ports to read the data from the instruments while being tested inside. This facility has been specifically designed for investigating the effect of water on the Martian surface. The core novelties of this chamber are: (1) its ability to simulate the Martian near-surface water cycle by injecting water multiple times into the chamber through a syringe which allows to control and monitor precisely the initial relative humidity inside with a sensor that can operate from vacuum to Martian pressures and (2) the availability of a high-intensity UV lamp, operating from vacuum to Martian pressures, within the chamber, which can be used to test material curation, the role of the production of atmospheric radicals, and the degradation of certain products like polymers and organics. For illustration, here we present some applications of the SpaceQ chamber at simulated Martian conditions with and without atmospheric water to (i) calibrate the ground temperature sensor of the Engineering Qualification Model of HABIT (HabitAbility: Brines, Irradiation and Temperature) instrument, which is a part of ExoMars 2022 mission. These tests demonstrate that the overall accuracy of the temperature retrieval at a temperature between −50 and 10 °C is within 1.3 °C and (ii) investigate the curation of composite materials of Martian soil simulant and binders, with added water, under Martian surface conditions under dry and humid conditions. Our studies have demonstrated that the regolith, when mixed with super absorbent polymer (SAP), water, and binders exposed to Martian conditions, can form a solid block and retain more than 80% of the added water, which may be of interest to screen radiation while maintaining a low weight. 

Place, publisher, year, edition, pages
MDPI, 2020. Vol. 20, no 14, article id 3996
Keywords [en]
space, environmental chamber, Mars simulation, vacuum, planetary atmosphere, space instrumentation
National Category
Aerospace Engineering
Research subject
Atmospheric Science
Identifiers
URN: urn:nbn:se:ltu:diva-80361DOI: 10.3390/s20143996ISI: 000554146200001PubMedID: 32708384Scopus ID: 2-s2.0-85088230630OAI: oai:DiVA.org:ltu-80361DiVA, id: diva2:1457294
Funder
The Kempe FoundationsKnut and Alice Wallenberg Foundation
Note

Validerad;2020;Nivå 2;2020-08-18 (alebob)

Available from: 2020-08-11 Created: 2020-08-11 Last updated: 2025-04-17Bibliographically approved
In thesis
1. A planetary chamber to investigate the thermal and water cycle on Mars
Open this publication in new window or tab >>A planetary chamber to investigate the thermal and water cycle on Mars
2022 (English)Doctoral thesis, comprehensive summary (Other academic)
Abstract [en]

The water processes that affect the upper layers of the surface of Mars are not yet fully understood. Describing the processes that may induce changes in the water content ofthe surface is critical to determine the present-day habitability of the Martian surface,understand the atmospheric water cycle, and estimate the efficiency of future water extraction procedures from the regolith for In-Situ-Resource-Utilization (ISRU). This PhD thesis describes the design, development, and plausible uses of a Martian environmental facility ‘SpaceQ chamber’ which allows to simulate the near surface water cycle.

This facility has been specifically designed to investigate the effect of water on the Martian surface. SpaceQ has been used to investigate the material curation and has demonstrated that the regolith, when mixed with super absorbent polymer (SAP), water, and binders exposed to Martian conditions, can form a solid block, and retain more than 80% of the added water, which may be of interest to screen radiation while maintaining a low weight. The thesis also includes the testing of HABIT operation, of theESA/IKI ExoMars 2022 robotic mission to Mars, within the SpaceQ chamber, underMartian conditions similar to those expected at Oxia Planum. The tests monitor the performance of the brine compartment, when deliquescent salts are exposed to atmospheric water.

In this thesis, a computational model of the SpaceQ using COMSOL Multiphysics has been implemented to study the thermal gradients and the near surface water cycle under Martian temperature and pressure experimental conditions. The model shows good agreement with experiments on the thermal equilibration time scales and gradients. The model is used to extrapolate the one-point relative humidity measurement of the experimental to each grid points in the simulation. This gives an understanding ofthe gradient in atmospheric water relative humidity to which the experimental samples such as deliquescent salts and Martian regolith simulants are exposed at different time intervals. The comparison of the thermal simulation and the experimental behavior of HABIT instrument tests, shows an extra internal heating source of about 1 W which can be attributed to the hydration and deliquescence of the salts exposed to Martian conditions when in contact with atmospheric moisture.

Finally, this thesis experimentally demonstrates that pure liquid water can persist for 3.5 to 4.5 hours at Mars surface conditions. The simulated ground captured 53% of the atmospheric water either as pure liquid water, hydrate, or brine. The result concludes  that the relative humidity values at night-time on Mars may allow for significant water absorption by the ground, which is released at sunrise. The water cycle dynamics near the surface is therefore always out of equilibrium. After frost formation, thin films of water may survive for a few hours. The results of this thesis about the water cycle on Mars, and about the interaction of atmospheric water with regolith and salts, have implications for the present-day habitability of the Martian surface and planetary protection policies.

Place, publisher, year, edition, pages
Luleå: Luleå University of Technology, 2022
Series
Doctoral thesis / Luleå University of Technology 1 jan 1997 → …, ISSN 1402-1544
Keywords
Mars, space chamber, ISRU, water cycle simulation, pure liquid water, habitability, heat transfer
National Category
Earth and Related Environmental Sciences
Research subject
Atmospheric science
Identifiers
urn:nbn:se:ltu:diva-89007 (URN)978-91-8048-018-5 (ISBN)978-91-8048-019-2 (ISBN)
Public defence
2022-04-06, A1545, Luleå, 09:30 (English)
Opponent
Supervisors
Available from: 2022-01-31 Created: 2022-01-30 Last updated: 2025-02-07Bibliographically approved

Open Access in DiVA

fulltext(3407 kB)519 downloads
File information
File name FULLTEXT01.pdfFile size 3407 kBChecksum SHA-512
d9d29df5742579127987ba03426e82abc09976884808276fe3e175a0b3873e9817f2060e51d03e8e2e8c7bed8dbd83fe8c9912549671fc4bd21dfbfb662da4d1
Type fulltextMimetype application/pdf

Other links

Publisher's full textPubMedScopus

Authority records

Vakkada Ramachandran, AbhilashIsrael Nazarious, MiracleMathanlal, ThasshwinZorzano, María-PazMartin-Torres, Javier

Search in DiVA

By author/editor
Vakkada Ramachandran, AbhilashIsrael Nazarious, MiracleMathanlal, ThasshwinZorzano, María-PazMartin-Torres, Javier
By organisation
Space Technology
In the same journal
Sensors
Aerospace Engineering

Search outside of DiVA

GoogleGoogle Scholar
Total: 520 downloads
The number of downloads is the sum of all downloads of full texts. It may include eg previous versions that are now no longer available

doi
pubmed
urn-nbn

Altmetric score

doi
pubmed
urn-nbn
Total: 381 hits
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf