 Original Article
 Open access
 Published:
On Modeling Drilling Load in Lunar Regolith Simulant
Chinese Journal of Mechanical Engineering volume 31, Article number: 20 (2018)
Abstract
Drilling and coring, as effective ways to obtain lunar regolith along the longitudinal direction, are widely applied in the lunar sampling field. Conventionally, modeling of drillsoil interaction was divided into soil cutting and screw conveyance processes, ignoring the differences in soil mechanical properties between them. To improve the modeling accuracy, a hypothesis that divides the drillsoil interaction into four parts: cuttings screw conveyance, cuttings extruding, cuttings bulldozing, and in situ simulant cutting, is proposed to establish a novel model based on the passive earth pressure theory. An iterative numerical calculation method is developed to predict the drilling loads. A drilling and coring testbed is developed to conduct experimental tests. Drilling experiments indicate that the drilling loads calculated by the proposed model match well the experimental results. The proposed research provides the instructions to adopt a suitable drilling strategy to match the rotary and penetrating motions, to increase the safety and reliability of drilling control in lunar sampling missions.
1 Introduction
Research on lunar regolith can enhance knowledge regarding lunar regolith composition and planetary history [1, 2]. Drilling systems are widely used for extraterrestrial subsurface regolith sampling, because they are appropriate tools to acquire regolith samples while maintaining their stratification along the longitudinal direction [3,4,5]. The mission of Chang’e5 lunar exploration project aims to obtain lunar subsurface regolith through a drilling and coring device, and return it to the Earth. Though the mechanical properties of the lunar regolith obtained by the Soviet Union and the United States have been analyzed and reported in the literature, the regolith materials at a specific site are not known [6, 7]. The drill tool should have operative performance to adapt to lunar regolith with different mechanical properties. Therefore, ground experiments must be conducted with the desired lunar regolith simulant to validate whether the drill tool can obtain an appropriate sample [1, 8]. The modeling of the drillsimulant interaction simulates the drilling mechanism, which is used to predict drilling load, and represents a fundamental reference to eventually design an appropriate drill tool and develop a suitable drilling strategy [9].
The finite element method (FEM) and discrete element method (DEM) have been used to develop the model of drillsoil interaction [9,10,11,12]. Because the FEM is a gridbased method, it cannot deal well with large deformation and postfailure problems. It may suffer from mesh distortion, resulting in an inaccurate solution and failure of computational convergence [1, 2]. Although the DEM does not have that limitation, the high computational cost restricts DEM application to smallscale or shortduration simulations [13].
Analytical models have also been used to predict the drilling load [9, 14,15,16,17,18,19,20]. The analytical model of drillsoil interaction was developed using the screw conveyance theory and soil shear rupture principle. The analysis of the soil rupture is based on the passive earth pressure theory, which has successfully been used to predict the bulldozing force [21, 22]. According to the shape and cutting rake angle of the blade, different cutting models have been proposed to describe the soil rupture mechanism [23,24,25,26]. These theories can be used as a fundamental reference for modeling drilltool interaction. The screw conveyance calculation, which is similar to the bulk solid screw conveyor design, can predict particle screw conveyance load and efficiency [27,28,29]. According to the screw diameters and the rotary speed of an auger, the centripetal force or the weight of particles are the main causes of auger conveyance [30, 31]. The rotary speed is always less than 300 r/min, and the diameters of the drill tool are generally limited below 50 mm in extraterrestrial exploration. For such orders of rotary speed and diameters, the weight of particles could be the main component that provides cuttings conveyance [30]. This study models the screw conveyance process based on a quasistatic analysis. In addition, in a significant number of previous works, the drillsoil interaction was simply divided into screw conveyance and soil cutting processes. The boundary conditions and soil mechanical property differences between these two processes were ignored in previous modeling of the drillsoil interaction. Thus, the calculated results, i.e., the summations of the screw conveyance load and soil cutting load, must either be further verified or only used in special situations.
The authors’ previous experiments demonstrated that it is difficult to predict the drilling load accurately when only the screwconveying load and soil shear rupture are considered during simulant drilling. The simulant rupture is accompanied by simulant chip flow during simulant drilling, which may significantly influence the drilling load. The boundary conditions and simulant mechanical property differences between the simulant cutting and the cuttings conveyance processes should be considered in the drillsimulant interaction model. In this study, according to the structure of the drill tool, the drillsoil interaction is divided into four parts: cuttings conveyance, chip extruding, chip bulldozing, and in situ simulant cutting. To simulate the drilling mechanism, a drillsimulant interaction model, considering the boundary conditions and simulant density difference among these four parts, is developed to predict the drilling load. Drilling experiments are conducted to validate the presented model.
The remainder of this paper is organized as follows. First, the lunar regolith simulant and drill tool used in this paper are introduced. Then, a simulantcuttings conveyance analysis is presented. Next, a drillsimulant interaction model is developed to predict the drilling load. Finally, drilling experiments are conducted to validate the proposed model and the results are presented.
2 Lunar Regolith Simulant and Drill Tool
To sample a lunar regolith along the longitudinal direction, it is necessary to design a special drill tool to adapt to the complex lunar environments. Ground drilling and coring experiments should be conducted with the lunar regolith simulant to validate the performance of the designed drill tool.
2.1 Lunar Regolith Simulant
The lunar regolith simulant was created using basaltic pozzolana collected from Nanjing, China. The mineral composition of pozzolana includes plagioclase, olivine, pyroxene, opaque mineral, and volcanic glass, which is similar to that of the lunar regolith from the Apollo 14 landing site [32]. The particlesize range of the simulant is 0.1–1 mm, and the median grain size is 0.41 mm [33]. According to the data on particle size distribution of lunar regolith, the particle size distribution band of the simulant matches the actual lunar regolith [34, 35].
The relative density of lunar regolith is generally low to medium in the shallow layer, and approaches the maximum value just 10–20 cm below the lunar surface [6, 36]. Additionally, for a drilling system, the regolith simulant with high relative density is the most challenging case in terms of overhead drilling load [37]. Therefore, the dense regolith simulant may be more suitable to test the drilling device. The dense simulant used in this paper was prepared by vibratory compaction. Physical property tests (following the SL2371999 standard procedure [38]) reveal that the density, specific gravity, relative density, internal friction angle, and cohesion are 2.14 g/cm^{3}, 2.94 g/cm^{3}, 98%, 35.1°, and 2.85 kPa, respectively [33].
2.2 Drill Tool
To acquire the regolith samples along the depth direction, the drill tool is hollow, as shown in Figure 1, and consists of a drill bit and an auger. The drill bit is used to crack the regolith and maintain the auger position. Four kentanium blades radially mounted on the drill bit are used to cut the regolith. The screw of the auger is used to convey the chips to the lunar surface. A coring device, which has been introduced in the literature, is installed in the hollow auger [33]. Because there is no relative sliding between the regolith and coring device, this coring manner can keep stratification of the regolith and has negligible effect on coring samples [39].
3 Simulant Cuttings Conveyance Analysis
In the authors’ previous experiments, the simulant cuttings filled the auger groove when drilling the dense simulant samples with a rotary speed below 200 r/min. However, the density of the chips varies with the drilling parameters (defined as a combination of penetrating speed and rotary speed in this paper) as shown in Figure 2. To explain this conveyance behavior, this section will analyze the screw conveying process, which is the foundation of the drillsoil interaction modeling.
The screw conveyor design assumes that the fictional force created by the centrifugal force is the main component that provides the forward motion of the particles [22, 31]. The rotary speed is always lower than 300 r/min (the rotary speed of the CE5 is limited below 200 r/min), and the diameter of the drill tool is generally limited below 50 mm (the diameter of the CE5 is limited below 32 mm) in the extraterrestrial exploration. With this order of the rotary speed and diameters, the centrifugal force may not be the main component that provides for the cuttings conveyance [30, 40]. This paper models the screw conveying process based on a quasistatic analysis. In view of the reduced auger groove height and the low motion speed of the chips, the flow of the chips in the auger groove can be assumed to be in the ideal critical state:

(1)
The flow of the cuttings is uniform, and the cuttings do not exchange the position in the vertical direction;

(2)
The granular vortex motion is ignored.
The in situ simulant is stirred by the drill bit into loose simulant cutting and conveyed to the surface where the drill tool begins to drill into the simulant. The remainder is collected into the sampling device. The penetrating motion is accompanied by the production of cuttings, and the rotary motion conveys the cuttings.
Based on the assumption of the chip flow, the kinematic analysis of the conveying action is depicted in Figure 3. According to the velocity diagram, the velocity of the simulant chips can be expressed as
where v is the velocity of the auger, v_{r} is the relative velocity of the chips to the auger surface, v_{s} is the absolute velocity of the chips, \(\omega\) is the angular velocity of the auger, n is the rotary speed of the auger, r_{1} is the radius of the auger, \(\alpha\) is the helix angle of the auger, and \(\beta\) is the helix angle of the conveying path of the chips.
Solving Eq. (1) gives
where v_{l} is the effective conveying component of the v_{s}, and v_{t} is the rotational component of the v_{s}.
The demand flux of cuttings conveyance under a penetrating speed is given by
where v_{p} is the penetrating speed, and r_{2} is the coring radius.
The flux of cuttings conveyance capacity of the auger:
where \(h_{\text{s}}\) is the thickness of the flight.
The drilling device can drill into the simulant smoothly when the volume of the chips produced by penetration (VCP) equals or is lower than the volume of cuttings conveyance capacity (VCCC), otherwise the drill will be blocked by the chips. To ensure a healthy drilling, the critical state of the conveying process can be expressed as
where \(\rho_{\text{i}}\) is the density of the in situ simulant, and \(\rho_{\text{d}}\) is the density of the chips.
To obtain \(\beta\), the mechanical analysis of the conveying action is carried out as shown in Figure 4. F_{f3} has two components: friction between the chips and in situ simulant, and cohesion of the chips. Because the chips in the auger groove are under a highflow condition, they can be regarded as a Molerus I soil, and the cohesion of the chips can be ignored. In the ideal particle conveying action, the forces are in equilibrium condition:
where F_{f3} is the frictional force between the chips and the in situ simulant, F_{f1} is the friction force between the chips and the auger groove inner surface, F_{f2} is the friction force between the chips and the auger blade, N is the supporting force from the auger blade, N_{2} is the supporting force that is vertical to the interface between the chips and the in situ simulant, G is the gravity of the chips, \(\phi\) is internal friction angle of the cuttings, and \(\varphi\) is the helix angle of the conveying path of the chips.
Solving Eq. (3) gives
where g is the gravitational acceleration, \(\delta_{\text{z1}}\) is the top normal stress as shown in Figure 5, \(\delta_{\text{z2}}\) is the bottom normal stress, \(\delta_{\text{y}}\) is the lateral normal stress, h is the height of the auger groove as shown in Figure 5, and ds is the infinitesimal length along the helix of the auger.
To simplify the modeling process, the drillsoil interaction model is developed in the critical state. According to Eqs. (2), (4), and (7), the conveyance analysis flowchart is shown in Figure 6: (1) using the parameters of the drill tool (as listed in Table 1), drilling parameters, and the shear strength of the simulant as inputs, calculate Q_{p}, (2) assign the initial value of ρ_{d}, and then calculate Q_{e}, (3) search the appropriate value of the ρ_{d} until Eq. (7) is satisfied, and (4) calculate the conveyance load according to Eq. (7).
The calculated results reveal a trend of higher cuttings conveyance density for higher ratio of penetrating speed to rotary speed (RPS), as shown in Figure 7. The VCP increases with the penetrating speed; and the VCCC is proportional to the rotary speed. As the VCP remains unchanged, the effective conveying speed decreases with the rotary speed. To balance the VCP and keep the healthy drilling, the conveying density and \(\beta\) increase to keep the VCCC constant. When the RPS remains unchanged, the increase in the VCP is proportional to the increase in the VCCC, resulting in unchanged conveying density. Therefore, the conveying density is determined by the RPS according to the conveying analysis.
Figure 8 shows the relation between the conveying load and the drilling parameters. As the RPS increases, the higher conveying density leads to the increase of the friction between the chips and in situ simulant, resulting in the increase of the conveying load. According to the mechanical analysis of the conveying action depicted in Figure 4, the auger withstands tension. Previous experiments indicated that the drill tool withstands pressure rather than tension. Moreover, the rotary torque of the calculated results is normally of 1.4–2.2 N·mm, which is three orders smaller than the order of the experimental results (0.1–1 N·m). Therefore, the conveying load is not the main drilling load during simulant drilling and coring. To predict the drilling load, the next section involves the division of the drillsimulant interaction into four parts, and subsequently, analyzing the drilling load in each part.
4 Modeling of DrillSimulant Interaction
Based on the screw conveying analysis, this section involves the development of the bitsimulant interaction model. Summarizing the analysis of the screw conveying process and bitsimulant interaction, the drillsimulant interaction model can be developed to predict the simulant drilling load, considering the boundary conditions between these two parts. According to the structure of the drill bit, the bitsimulant interaction is divided into three parts (as shown in Figure 9): chip extruding, chip bulldozing, and in situ simulant cutting. The model of bitsimulant interaction is based on the hypothesis as follows:

(1)
The simulant is an isotropic, rigidplastic material;

(2)
Because the penetrating speed and the rotary speed are low, the drilling process is regarded as a quasistatic process.
4.1 Extruding Load Analysis
The drill tool conveys the chips to the auger in the extruding part, ensuring that the auger conveys the chips with appropriate conveying density under given drilling parameters. Because the helix angle in this part is 75°, it is difficult to convey the chips in a screw conveying manner. The model of the extruding part is based on the hypothesis that the chips are extruded to the auger. According to the mechanical analysis of the extruding process (as shown in Figure 10), the force equilibrium equation of the chips in the extruding part is expressed as follows:
where F_{1} is the extruding force, F_{s} is the friction force between the chips and the in situ simulant, \(\alpha_{1}\) is the helix angle of the extruding part, \(\beta_{1}\) is the helix angle of the conveying path of the chips in the extruding part, F_{f} is the friction force between the chips and the drill bit, N_{e} is the supporting force from the drill bit, G_{e} is the gravity of the chips in the extruding part, L_{1} is the arc length of the cross section of the drill bit in the extruding part, L_{2} is the arc length of the cross section of the extruding part at the interface between the chips and the in situ simulant, h_{e} is the height of the extruding part, and ds_{e} is the infinitesimal length along the helix of the auger in the extruding part.
To ensure healthy drilling, the volume of the cuttings conveyance capability is equal to the demand volume of the cuttings conveyance under a given penetrating speed. \(\beta_{1}\) is determined by the following equation:
where v_{er} is the relative velocity of the chips to the drill bit in the extruding part, and S_{s} is the sectional area of the extruding part.
According to Eqs. (8) and (9), Figure 11 shows the relation between the extruding load and drilling parameters when the penetrating speed is 85 mm/min. The extruding force of the calculated results is normally of the order of 7.5–11.5 mN, which is three orders smaller than the magnitude of the penetrating force in the drilling experiments (with order of 3–300 N). The following subsection discusses other parts of the bitsimulant interaction.
4.2 Bulldozing Load Analysis
The drill bit of the bulldozing part bulldozes the chips, and conveys the chips to the extruding part. The drilling loads of the bulldozing part are generated from the following parts: (1) compression of the loose chips into chips with conveying density by the drill bit, (2) the friction between the drill bit and the chips, and (3) the friction between the chips and the in situ simulant. Because the chips are the Molerus I soil, the analysis of the chips in the bulldozing part is based on the Walker analysis method, as shown in Figure 12 [41].
The compression of the chips in the bulldozing part is similar to the process of confined compression. The force that compresses the loose chips into the chips with conveying density, is determined by confined compression tests, which were conducted using a triaxial test system as shown in Figure 13 (following the SL2371999 standard procedure [38]). The relation between the compression pressure and the density of the simulant density is shown in Figure 14 and can be fitted as follows [23]:
where P is the compression pressure, and \(\rho\) is the density of the simulant.
According to the mechanical analysis of the bulldozing part, the force equilibrium equation of the simulant in the bulldozing part can be expressed as follows:
where P_{r} is the pressure on the bottom of the bulldozing part, \(\beta_{2}\) is the penetrating helix angle of the drill bit external cylinder, \(\beta_{3}\) is the penetrating helix angle of the drill bit inner cylinder, \(\tau_{\text{f}}\) is the shear stress between the chips and the in situ simulant, \(\sigma_{\text{r}}\) is the normal stress, which is vertical to the interface of the chips and the in situ simulant, S_{r1} is the external area of the bulldozing part, S_{r2} is the internal area of the bulldozing part, and k_{k} is the Walker constant.
The friction shear stress between the chips and the bit can be expressed as
Summarizing Eq. (11) and Eq. (12), the weight on bit (WOB) of the bulldozing part is expressed as
The rotary torque of the bulldozing part is expressed as
According to Eqs. (13) and (14), Figure 15 shows the relation between the bulldozing load and the rotary speed when the penetrating speed is 85 mm/min. As the penetrating speed remains unchanged, the VCP keeps constant. To ensure the healthy drilling, the VCCC should remain unchanged to balance the VCP. When the rotary speed decreases, the conveying density and \(\beta\) increase to keep the VCCC constant. The loose chips are compressed into the cuttings with conveyance density by the drill bit in the bulldozing part. The bulldozing load increases with the conveyance density. Therefore, as the penetrating speed keeps constant, a lower rotary speed leads to higher bulldozing load.
4.3 Cutting Load Analysis
The cutting depth of the blade on the drill bit is generally 0–0.5 mm in the planetary drilling, which is far smaller than the width of the blade [23]. The soil failure can be assumed to take place in a twodimensional field during the cutting process [21, 23, 42]. Because the simulant is a type of a granular material, shear rupture is the major rupture method during cutting [19,20,21]. Additionally, the simulant in the cutting part withstands the surcharge load from the bulldozing part. The upperbound limit method is suitable to calculate the cutting force with the blade rake angle of 90°, and is used to predict simulant cutting force, as shown in Figure 16 [42]. The region ABC is a triangular zone, which is governed by simulanttool friction. The region ACD is a logarithmic spiral mixed region. The region ADE is also a triangular zone and is assumed to be a Rankine zone.
In Figure 16, v_{0} is the velocity of the blade, v_{2} is the velocity of ABC, v_{3} is the velocity of ACD, v_{4} is the velocity of ADE, W_{1} is the weight of ABC, W_{2} is the weight of ACD, and W_{3} is the weight of ADE.
The upperbound limit model is solved by the principle of virtual work, and can be expressed as follows:
The equivalent factors are as follows:
where F_{3} is the cutting force, H is the cutting depth, \(\gamma\) is the bulk density of the in situ simulant, c is the apparent cohesion of the in situ simulant, q is the surcharge pressure, w is the width of the bit blade, \(\alpha_{2}\) is the rake angle of the blade, \(\theta\) is the angle of the region ABC, \(\psi\) is the angle of the region ACD, \(\phi_{1}\) is the internal friction angle of the in situ simulant, and \(\delta_{1}\) is the angle of simulantblade friction.
According to the motion of the drill tool, the cutting depth is expressed as
where \(n_{\text{c}}\) is the number of blades in the drill bit.
The passive earth pressure is expressed as
Because \(\alpha_{2}\) is 90°, the WOB of the cutting part is expressed as
The rotary torque of the cutting part is expressed as
According to Eqs. (15), (19), (21), and (22), Figure 17 shows the relation between the cutting force (contains the rotary torque and the WOB of the cutting part) and the rotary speed when the penetrating speed is 85 mm/min (the regions A and B represent the loads influenced by the surcharge pressure and cutting depth, respectively). As the RPS increases, indicating an increase in the cutting depth and surcharge pressure, the drilling loads increase.
The calculated results indicate that the effect of the surcharge pressure on the cutting force is greater than that of the cutting depth. When the RPS is higher than 0.7, the cutting force caused by the surcharge pressure is the main load. Therefore, the boundary condition has significant effect on the drilling load and must be considered in the modeling process.
4.4 Drilling Load Analysis
Summarizing the aforementioned analysis, the calculation flowchart of the drilling load is depicted in Figure 18, and the parameters of the drill bit are listed in Table 2. The calculation of the drilling load is based on the screw conveying analysis, and considers the boundary condition among the conveyance part, extruding part, bulldozing part, and simulant cutting part. The bulldozing loads are the major drilling loads, and the cutting loads are secondary, as shown in Figure 19 (the region A represents the bulldozing loads, B represents the cutting loads, and C represents the conveyance and extruding loads). The major part of the WOB is caused by the force that compresses the loose cuttings into the cuttings with conveyance density. The rotary torque is mainly produced by the friction between the cuttings and in situ simulant, and the friction between the drill bit and cuttings in the bulldozing part.
5 Experimental Verification
To validate the developed model, experiments were performed using a drilling and coring testbed equipped with a base of the testbed, rotary unit, penetrating unit, and lunar regolith simulant bin, as shown in Figure 20. The rotation of the drill is achieved by an AC servo motor with a 7:1 gearhead via a pair of gears with reduction ratio of 60:54. The rotary unit can be vertically actuated along two sliding guides at a desired speed by using a penetrating motor via chains. The control system of the testbed collects the realtime data and controls the drilling parameters during the drilling process. The sensors in the testbed are sixaxis force/torque sensors for the rotary torque and WOB, travel switches, and a magnetic scale for penetrating depth. The lunar regolith simulant bin is used to hold the lunar regolith simulant.
Previous experiments (drilling at a length of 0–2.3 m) indicated that the drilling loads increase significantly in the shallow layer and approach a steady value at a length of z > 50 mm (as shown in Figure 21; with the rotary torque and the WOB of 1.2 Nm and 100.0 N). Because the drilling loads are steady in the deep layer, the drilling length for each experiment was 300 mm from the surface of the lunar soil simulant to make the experiments more convenient to perform. The simulant sample for each experiment was prepared by fivelayer simulant vibratory compaction [33]. The control system collected the sensor data with the nominal sampling rate of 500 Hz. To ensure repeatability of the experiments, each experiment was repeated five times, and the results are presented as their mean value of the steady drilling loads in the deep layer.
The calculated results of the drilling load match well the experimental results, as shown in Table 3. The order of the calculated rotary torque is consistent with the order of the experimental results. As the rotary speed is lower than 200 r/min, the experimental results demonstrate that the drill loads are determined by the RPS; this is consistent with the prediction of the proposed model. When the RPS is higher than 1, the drilling loads increase significantly with the increase of RPS. As the penetrating speed remains unchanged, indicating a constant VCP, a lower rotary speed leads to lower effective screw conveying speed. To balance the VCP, \(\beta\) and conveying density of the chips in the auger increase to keep the VCCC constant. According to the analysis of the model, the conveying density of the chips is high when the RPS is higher than 1, resulting in serious bit jamming; this is the cause of high drilling loads. The proposed model can explain the bit jamming during simulant drilling. The experimental and the calculated results indicate that the drilling loads increase smoothly when the RPS is lower than 1. In terms of the drilling load, selection of an appropriate RPS in the range of 0–1 is suggested when drilling the dense simulant using the drill tool presented in this paper.
6 Conclusions

(1)
According to the structure of the drill tool, the interaction between the drill tool and lunar regolith simulant is divided into four parts: cuttings screw conveying, chip extruding, chip bulldozing, and in situ simulant cutting. Considering the boundary condition and simulant density difference among these four parts, a drillsimulant interaction model is developed to predict the drilling load during simulant drilling, based on the screw conveying and the passive earth pressure theory.

(2)
The mechanical analysis of each part demonstrates that the boundary conditions among these four parts cannot be ignored in the modeling of drillsimulant interaction. According to the analysis of the model, the bulldozing loads include the major drilling loads produced by chip compression, friction between the chips and the in situ simulant, and friction between the drill bit and chips.

(3)
A comparison of the drilling experiments and the calculated results demonstrates that the model can effectively predict the drilling load during simulant drilling. With the model, the design of drill tool and development of drilling strategy can be facilitated by a cyclic analysis of drilling load before prototypes are developed for ground drilling tests.

(4)
The main mission of the drilling system is to acquire an appropriate sample. While the drilling loads are low when the RPS is lower than 1, the mass of the coring sample may be low in this range. Combined with the drillsimulant interaction model, in future work, a model for predicting the coring mass should be developed to optimize the drilling parameters.
References
Y BarCohen, K Zacny. Extraterrestrial drilling and excavation. Weinheim: WileyVCH, 2009.
I A Crawford, K H Joy. Lunar exploration: opening a window into the history and evolution of the inner solar system. Philosophical Transactions of the Royal Society A  Mathematical, Physical and Engineering Sciences, 2014, 372: 1–21.
F Poletto, P Magnani, R Gelmi, et al. Seismic while drilling (SWD) methodology in support to moon subsurface stratigraphy investigations. Acta Astronautica, 2015, 110: 99–114.
T Zhang, Y H An, X L Ding. Device design and implementation method of lunar soil simulant vacuum test. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(11): 2110–2115. (in Chinese)
B J Glass, A Dave, C P Mckay, et al. Robotics and automation for “icebreaker”. Journal of Field Robotics, 2014, 31: 192–205.
G H Heiken, D T Vaniman, B M French. The lunar regolith. Cambridge: Cambridge University Press, 1991.
C Pitcher, N Komle, O Leibniz, et al. Investigation of the properties of icy lunar polar regolith simulants. Advances in Space Research, 2016, 57: 1197–1208.
X M Shi, Q Q Quan, Z Q Deng, et al. DMTbased estimation of mechanical properties for subsurface lunar soil simulant. Journal of Aerospace Engineering, 2016, 29(4): 040160031–0401600310.
A E Finzi, M Lavagna, G Rocchitelli. A drillsoil system modelization for future mars exploration. Planetary and Space Science, 2004, 52: 83–89.
T X Liu. Research on lunar soil drilling dynamics based on the discrete element method. Harbin: Harbin Institute of Technology, 2015. (in Chinese)
X H Zhu, Y J Jia. 3D mechanical modeling of soil orthogonal cutting under a single reamer cutter based on druckerprager criterion. Tunnelling and Underground Space Technology, 2014, 41: 255–262.
W Chen, T Qiu. Simulation of earthquakeinduced slope deformation using SPH method. International Journal for Numerical and Analytical Methods in Geomechanics, 2014, 38: 297–330.
J Wang, D Chan. Frictional contact algorithms in SPH for the simulation of soilstructure interaction. International Journal for Numerical and Analytical Methods in Geomechanics, 2014, 41: 747–770.
X M Shi, D G Jie, Q Q Quan, et al. Experimental research on lunar soil simulant drilling load analysis. Journal of Astronaytics, 2014, 35: 648–656. (in Chinese)
Y Tian, D W Tang, Z Q Deng, et al. Drilling power consumption and soil conveying volume performances of lunar sampling auger. Chinese Journal of Mechanical Engineering, 2015, 28(3): 451–459. (in Chinese)
L L Wang. Parameters optimization and reliability analysis of lunar drilling. Beijing: Beijing Institute of Technology, 2015. (in Chinese)
Q Q Quan, J Y Tang, F P Yuan, et al. Drilling load modeling and validation based on the filling rate of auger flute in planetary sampling. Chinese Journal of Aeronautics, 2017, 30: 434–446.
Z Q Liu, L L Wang, W R Wu, et al. Effect of structure parameters of drill bit on mechanical performances of lunar automatic drill sampling mechanism. Journal of Astronautics, 2015, 36(12): 1339–1347. (in Chinese)
L L Wang, Z Q Liu, W R Wu, et al. Analysis of drill stem structural and kinematic parameters of lunar drilling sampling mechanism. ACTA Aeronautica et Astronautica Sinica, 2016, 37(2): 738–748. (in Chinese)
L L Wang, Z Q Liu, W R Wu, et al. Multiobjective optimization of drill stem’s motion parameter of lunar automatic drill sampling mechanism. Journal of Astronautics, 2015, 36(6): 723–730. (in Chinese)
M Esmaeili, A Ivanovic. Analytical and numerical modelling of nondriven disc on friction material. Computers and Geotechnics, 2015, 68: 208–209.
R H King, V Susante, A Gefreh. Analytical models and laboratory measurements of the soiltool interaction force to push a narrow tool through JSC1A lunar simulant and ottawa sand at different cutting depths. Journal of Terramechanics, 2011, 48: 85–95.
R J Godwin. A review of the effect of implement geometry on soil failure and implement forces. Soil & Tillage Research, 2007, 97: 331–340.
P D Gupta, C P Gupta, K P Pandey. An analytical model for predicting draft forces on convextype wide cutting blades. Soil & Tillage Research, 1989, 14(2): 131–144.
R J Godwin, M J O’Dogherty. Integrated soil tillage force prediction models. Journal of Terramechanics, 2007, 44(1): 3–14.
E Mckyes, O S Ali. The cutting of soil by narrow blades. Journal of Terramechanics, 1977, 14(2): 43–58.
A W Roberts, A H Willis. Performance of grain augers. Proceedings of the Institution of Mechanical Engineers, 1962, 176: 165–194.
M Mellor. Mechanics of cutting and boring. Part 7. Dynamics and energetics of axial rotation machines. REL Report 81–26, Mississippi: Office of the Chief of Engineers, 1981.
K A Zacny, G A Cooper. Methods for cuttings removal from holes drilled on Mars. International Journal of Mars Science and Exploration, 2007, 3: 42–56.
A W Roberts. The influence of granular vortex motion on the volumetric performance of enclosed screw conveyors. Powder Technology, 1999, 104: 56–67.
J Dai, R Grace. A model for biomass screw feeding. Powder Technology, 2008, 104: 40–55.
J C Laul, J J Papike, S B Simon. The Apollo 14 regolith: Chemistry of cores 14210/14211 and 14220 and soils 14141, 14148 and 14149. Journal of Geophysical Research, 1982, 87: A247–A259.
C B Chen, Q Q Quan, Z Q Deng, et al. Vibratory compaction method for preparing lunar regolith drilling simulant. Advances in Space Research, 2016, 58: 145–154.
J K Mitchell, W N Houston, R F Scott, et al. Mechanical properties of lunar soil: Density, porosity, cohesion, and angle of internal friction. Proceedings of the Third Lunar Science Conference, The MIT Press, 1972, 3: 3235–3253.
W D Carrier. Lunar soil grain size distribution. The Moon, 1973, 6: 250–263.
J K Mitchell, W N Houston, W D Carrier. Apollo soil mechanics experiment S200, Final report NASA Contract NAS 911266. Berkeley: Space Sciences Laboratory, 1974.
T P Gouache, C Brunskill, G P Scott, et al. Regolith simulant preparation methods for hardware testing. Planetary and Space Science, 2010, 58: 1977–1984.
The Ministry of Water Resources of the People’s Republic of China. SL2371999 Specification of soil test. Beijing: Standards Press of China, 1999.
Q Q Quan, C B Chen, Z Q Deng, et al. Recovery rate prediction in lunar regolith simulant drilling. Acta Astronautica, 2017, 133: 121–127.
D M Zhao, D W Tang, X Y Hou, et al. Soil chip convey of lunar subsurface auger drill. Advances in Space Research, 2016, 57: 2196–2203.
R M Nedderman. Statics and Kinematics of Granular Materials. Cambridge: Cambridge University Press, 1992.
W F Chen, X L Liu. Limit analysis in soil mechanics. Amsterdam: Elsevier, 1990.
Authors’ contributions
QQQ and CBC carried out the theoretical analysis and experimental studies and drafted the manuscript. ZQD, JYT, and DWT participated in the sequence alignment and manuscript revision. All authors read and approved the final manuscript.
Authors’ Information
QiQuan Quan born in 1983, is currently an associate professor at State Key Laboratory of Robotics and System, Harbin Institute of Technology, China. He received his PhD degree from Ritsumeikan University, Japan, in 2010. His research interests include rotarypercussive ultrasonic drill, Martian UAV, and sensors based on SAW.
ChongBin Chen born in 1986, is currently a PhD candidate at State Key Laboratory of Robotics and System, Harbin Institute of Technology, China. He received his master’s degree from Nanjing University of Science and Technology, China, in 2012. His area of research includes automated planetary sampling.
ZongQuan Deng born in 1956, is currently a professor at Harbin Institute of Technology, China. He received his master’s degree from Harbin Institute of Technology, China, in 1984. His research interests include planetary rover, deployable space mechanisms, and planetary sampling technology.
JunYue Tang born in 1989, is currently a PhD candidate at State Key Laboratory of Robotics and System, Harbin Institute of Technology, China. He received his master’s degree from Harbin Institute of Technology, China, in 2014.
DeWei Tang born in 1966, is currently a professor at Harbin Institute of Technology, China. He received his PhD degree at Harbin Institute of Technology, China, in 2000. His research interests include inpipe robots, automated planetary sampling technology.
Acknowledgements
Supported by National Natural Science Foundation of China (Grant No. 61403106).
Competing interests
The authors declare that they have no competing interests.
Ethics approval and consent to participate
Not applicable.
Publisher’s Note
Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
Open Access This article is distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution, and reproduction in any medium, provided you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license, and indicate if changes were made.
About this article
Cite this article
Quan, QQ., Chen, CB., Deng, ZQ. et al. On Modeling Drilling Load in Lunar Regolith Simulant. Chin. J. Mech. Eng. 31, 20 (2018). https://doi.org/10.1186/s1003301802078
Received:
Accepted:
Published:
DOI: https://doi.org/10.1186/s1003301802078