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Development of a new test bench dedicated to adhesion characterization of lunar dust simulants
in space environment
ISMSE 14th – ICPMSE 12th
Pauline Oudayer – ONERA/DPHY/CSECo-authors: Jean-Charles Matéo-Vélez(1), Célia Puybras(2), Jean-François
Roussel(1), Sébastien Hess(1), Pierre Sarrailh(1) and Gaël Murat(1)
(1) ONERA, the French Aerospace Lab(2) La prépa des INP, Institut National Polytechnique
Context – Dust contamination on Mars
2Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
Photo of before and after dust contamination of Opportunity roverCredit: NASA/JPL-Caltech/Cornell Univ./Arizona State Univ.
• Dust cleaning improved the rover lifetime• Wind can be simultaneously decontaminant and contaminant factor
January 2014 March 2014
• Opportunity and Curiosity missions feedback: dust contamination happened• Mars has its own atmosphere and dust• Wind → « cleaning event »
Context - Origins of dust contamination on the Moon
3Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
Credit: NASAApollo archives
Before After
• Human activity - Dust contamination occured due to astronauts work
Surface obscurations
Space suit anomalies Lunar module contamination
Context - Surface properties of the Moon
4Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
• Moon surface is covered in dust layer called regolith (< 1cm)• Lunar dust is the < 20 µm portion of the regolith• Results from differents processes:
• Impact of large and small meteoroids• Steady bombardment of particles from the Sun
• Thickness between 5 m (mare areas) and up to 15 m (highlands)• Dust adheres a lot and lead to heavy dust contamination
Moon surface (Apollo 11)Credit: NASA
5Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
Context - Origins of dust contamination on the Moon
• Bombardment of meteroids• Charging environment around the Moon
• Electron recollection from solar wind → negatively charged surface• Day-side: photoemission phenomena → positively charged surface• At the night/day frontier: electrostatically lofted dust (Horizon Glow)
Photo of the Horizon Glowtaken by the Clementine probe
Context – Origins of dust contamination on Earth
6Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
• To a smaller extent, dust contamination may still appear in clean rooms
• « Pre-flight » contamination
Objectives
• Understand complex adhesion physical phenomena
• Develop and validate a new experimental setup dedicatedto adhesion force quantification
• Use it under conditions representative of the lunar chargingenvironment
7Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
Table of contents
• Reminder on adhesion force
• Development of a new setup at ONERA in the DROP facility
• Preliminary results
• Conclusions and perspectives
8Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
Van der Waals adhesion force
• Van der Waals force resulting of dipolar interactions: London, Debye, Keesom
• For an interaction between a smooth sphere and substrate in vacuum:
• A = Hamaker constant [J]. Typical values: 10-20; 10-19 J • Rp = particle radius [m]• d = minimum separation distance [m]. Typical value: a few angstroms
→ Estimation of all three parameters is challenging
9Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
���� ��
��²∝Rp
Particle
Substrate
Shape of lunar samples
10Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
Credit: Liu, 2011 (and references hereby)
SEM photos of lunar dust samples
• Irregular shape
• Rugged forms
• « somewhatelongated »
• Asperities
• Porous
Effect of roughness on adhesion force
11Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
��� ���
6���
1
1 �58�����
λ²
�1
1 �1,82���
��
�
• Previous equation only supposed an interaction with a smooth surface
• (Rabinovich, 2000) proposed a more precise expression for Fadwhere the substrate has a roughness rms
→ As substrate roughness increases, adhesion force decreases
Rp
Effect of roughness on adhesion force
• Surface treatments (ion bombardment, coatings… ) have been used in order to increase a surface rougness
12Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
Credit: Devaud, 2014
Images of virgin (left) and treated (right) black Kapton sample
AFM
Photos after dustdeposition and removal
Effect of roughness on adhesion force
• Dust adhesion force quantification done using AFM methodbetween a smooth tungsten sphere and varying roughnesssubstrates
13Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
Courtesy of S. Peillon (paper submitted)
Development of a new setup
14 Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
Credit: Mittal, 2015
Credit: http://research.iitgn.ac.in/
Existing setups providing adhesion force measurement:
Credit: Mizes, 2008
AFM (atomic force microscope)
Shear strengh
Centrifugal force
Experimental facility
15Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
• Quantifying adhesion force → use of centrifugal force• Vacuum chamber called DROP (Dust Regolith or Particles)• Vacuum: < 10-6 mbar• External motor goes from 100 rpm to 1500 rpm• Measurement ex-situ: binocular magnifier
Vacuum chamber
External motor Rotor
Sample preparation
16Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
• Simulant used: DNA-1• > 140 µm• [50 µm, 140 µm]• [25 µm, 50 µm]• < 25 µm
• Density: 2,9.103 kg/m3
• Substrates: aluminum and graphite samples (size: 20x20 mm, 2 mm thick)
Dust
Substrate
• In order to improve the contrast, a black dot is printed on the substrate(scale: 200µm)
Rotor
SEM photos of DNA-1 simulant
Adhesion forces measurements
17Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
• Assumption: dust particles are spherical
• Centrifugal force:
�( �ω²� ∝ ��*
m: particle mass [kg]ω: angular speed of rotation [rad/s]R: rotor radius [m]
• Adhesion force (just before particle detachment) :
��� − �(,,�- � �. ~− �(,,�- as01
02,3456 108�
Individual grains (aluminum substrate), scale=100µm:
Particle mean size: 22 µmFad ~ 20-30 nN
Adhesion forces measurments – Preliminary results
18Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
Before
Before After 1500 rpm
After 1500 rpm
Particle mean size: 35 µm
Comparison with literature
19Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
Interaction between a W sphereand a rough tokamak surface
Interaction between a W sphere and a smooth W surface (rms = 15 nm)
Interaction between a W sphereand a rough W surface (rms = 750 nm)
Present work
Interaction between dust simulant and a virgin and a treated surface
• Use of centrifugal force as a method of determining adhesion force is reachable under vacuum and for lunar dust simulant down to at least 20 microns in diameter
• Limitation of the system: only data of none and fully-spun sample → overestimation of the adhesion force
• Needs improvement to reach in-situ optical measurements in real-time and high resolution optical measurements
• Obtained results are in agreement with literature• Substrate roughness has a big importance in the adhesion force
Observations of dust clusters on the graphite substrate, scale=100µm:
Conclusions
20Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
Before BeforeAfter 1500 rpm After 1500 rpm
Perspectives
21Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
• Test bench validation using clearly identified situations: • Use of spherical samples• Use of substrates of varying roughnesses
• Take into account electrostatic forces in space environment and quantifytheir contribution to dust adhesion and contamination using electron gun and VUV source
SEM photos of glass particlesSize: 30±20 µm
Acknowledgments
“The major issue the Apollo astronauts pointed out was dust,dust, dust.”
22Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
Professor Larry Taylor, University of Tennessee
Authors would like to thank CEA Cadarache and IRSN forproviding data and discussions
Some references
23Development of a new test bench dedicated to adhesion characterization of lunar dust simulants in space environment
• Sandra A. Wagner, “The Apollo Experience Lessons Learned for Constellation Lunar Dust Management.” 17-Jan-2008.
• M. Horanyi et al., “A permanent, asymmetric dust cloud around the Moon,” Nature, vol. 522, no. 7556, pp. 324–326, Jun. 2015.
• J. N. Israelachvili, Intermolecular and surface forces, 3. ed. Amsterdam: Elsevier, Acad. Press, 2011.• Y. I. Rabinovich, J. J. Adler, A. Ata, R. K. Singh, and B. M. Moudgil, “Adhesion between Nanoscale
Rough Surfaces,” J. Colloid Interface Sci., vol. 232, no. 1, pp. 10–16, Dec. 2000.• A. Autricque et al., “Simulation of W dust transport in the KSTAR tokamak, comparison with fast camera
data,” Nucl. Mater. Energy, vol. 12, pp. 599–604, Aug. 2017.• M. Soltani and G. Ahmadi, “Detachment of rough particles with electrostatic attraction from surfaces in
turbulent flows,” J. Adhes. Sci. Technol., vol. 13, no. 3, pp. 325–355, Jan. 1999.• A. Dove, G. Devaud, X. Wang, M. Crowder, A. Lawitzke, and C. Haley, “Mitigation of lunar dust adhesion
by surface modification,” Planet. Space Sci., vol. 59, no. 14, pp. 1784–1790, Nov. 2011.• S. Peillon, A. Autricque, F. Gensdarmes, C. Grisolia, “Adhesion of tungsten microspheres on rough
tungsten surfaces using Atomic Force Microscopy.” Submitted to Journal of Colloid and Interface Science.
• K. L. Mittal and R. Jaiswal, Eds., Particle Adhesion and Removal: Mittal/Particle. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2015.
• G. Devaud, C. Haley, C. Rockwell, and A. Fischer, “Surfaces that shed dust: unraveling the mechanisms,” presented at the SPIE Optical Engineering + Applications, San Diego, California, United States, 2014, p. 919603.
• J. Gaier, D. Waters, B. Banks, R. Misconin, and M. Crowder, “Evaluation of Surface Modification as a Lunar Dust Mitigation Strategy for Thermal Control Surfaces,” in 41st International Conference on Environmental Systems, Portland, Oregon, 2011.