AGH University of Krakow · Faculty of Drilling, Oil and Gas
COSMODRILL · Scientific Club

COSMOBOSS

A Tracked Micro-Rover for Drilling Under Low Lunar Gravity

AuthorsJakub Zalewski · Aleksander Roratowski
Supervisorsdr inż. Przemysław Toczek · dr inż. Krzysztof Skrzypaszek
FacultyDrilling, Oil and Gas · AGH University of Krakow
SGEM 2026 · XXVI Int. Multidisciplinary Scientific GeoConference · 4-13 July 2026 · Albena Resort & Spa, Bulgaria
AGHWNiG
AGH University of Krakow
Faculty of Drilling, Oil and Gas
#COSMOBOSS · Tracked Micro-Rover
Slide 01 · Background

Context: Rovers and Miniaturisation

Uncrewed, remotely operated rovers have explored other celestial bodies since 17 November 1970, when the Soviet Lunokhod 1 landed on the Moon. Since then, nine rovers in total have operated on the lunar surface - including three crewed Lunar Roving Vehicles of the Apollo programme.

Yet none used continuous tracks: tracks have considerably greater mass than wheels, drastically increasing mission cost. In parallel, a strong miniaturisation trend produced palm-sized and CubeSat-scale robots that cut launch mass. The #COSMOBOSS micro-rover follows this trend - but departs from convention by adopting a tracked chassis.

Timeline at a glance

  • 1970 - Lunokhod 1, first uncrewed lunar rover
  • 9 rovers total operated on the Moon
  • 3 crewed Apollo Lunar Roving Vehicles
  • 0 ever used continuous tracks

Tracks were excluded for one reason: their mass. This work turns that drawback into the central advantage.

SGEM 2026 · Albena, Bulgaria #COSMOBOSS02 / 16
◉ Interactive · gravity → drilling depth
AGHWNiG
AGH University of Krakow
Faculty of Drilling, Oil and Gas
#COSMOBOSS · Tracked Micro-Rover
Slide 02 · The central limitation

The Core Problem: Weight-on-Bit on the Moon

Reduced gravity and the absence of an atmosphere make it hard to drill deeper than 1-2 m on the Moon. The force pressing the bit into the formation - the weight-on-bit (WOB) - is fundamentally limited by the low weight of any equipment.

  • Moon gravity ≈ 1/6 of Earth
  • 1 kg on Earth → only ~167 g of weight on the Moon
  • Solution: deliberately add mass through tracks

Gravity → achievable drilling depth

g = 9.81 m/s² WOB factor 1.00×
Achievable depth ≈ deep

On the Moon, the same rig reaches only the 1-2 m band - lifting effective weight (heavier tracks) is the direct lever on WOB.

SGEM 2026 · Albena, Bulgaria #COSMOBOSS03 / 16
◉ Interactive · wheel vs track
AGHWNiG
AGH University of Krakow
Faculty of Drilling, Oil and Gas
#COSMOBOSS · Tracked Micro-Rover
Slide 03 · Two complementary advantages

Why Tracks? Heavy at the bit, light at the patch

  • ① More mass → more WOB. Tracks add the very mass that raises weight-on-bit - the limiting factor for borehole depth under low lunar gravity.
  • ② Constant, low ground pressure. Continuous tracks spread the weight over a much larger contact area, lowering nominal ground pressure and reducing sinkage and motion resistance on loose soil.

The two effects are complementary: tracks let the rover be heavy where heaviness helps (at the bit) while staying light where heaviness harms (at the contact patch).

Contact patch & sinkage on loose regolith

Contact area large Sinkage low

Same vehicle weight - the wheel concentrates it on a small patch and digs in; the track distributes it and stays on top.

SGEM 2026 · Albena, Bulgaria #COSMOBOSS04 / 16
AGHWNiG
AGH University of Krakow
Faculty of Drilling, Oil and Gas
#COSMOBOSS · Tracked Micro-Rover
Slide 04 · The medium

Regolith: The Extreme Environment

Regolith is the loose, weathered layer of dust and crushed rock covering celestial-body surfaces; on the Moon it forms a thick layer, in places several metres deep.

Its grains are extremely fine and unusually sharp - with no atmosphere, there is no wind to polish them. The resulting abrasive dust damaged equipment as early as Apollo 11. These properties make trafficability and the avoidance of sinkage central design problems - and motivate the experimental study of the track-regolith interaction reported here.

Why regolith is hostile

  • Deep - locally several metres of loose material
  • Fine & sharp grains - no wind-polishing
  • Abrasive dust - equipment damage since Apollo 11
  • Drives trafficability & anti-sinkage design

Sharp angular grains lock together - high internal friction, but easy to dig into.

SGEM 2026 · Albena, Bulgaria #COSMOBOSS05 / 16
AGHWNiG
AGH University of Krakow
Faculty of Drilling, Oil and Gas
#COSMOBOSS · Tracked Micro-Rover
Slide 05 · Architecture

Rover Design: Key Features

Envelope

Remotely operated, not exceeding 20 × 20 × 30 cm, running on two independently driven tracks for enhanced manoeuvrability and the ability to turn in place.

Acoustic sensing

A turret of ultrasonic distance sensors on a movable platform, rotation range −90° to +90° relative to travel direction.

Magnetic sensing

Hall-effect sensors at front and rear detect local magnetic-field disturbances, indicating ferromagnetic material.

Real-time mapping

Terrain data are processed so a program builds, in real time, a map with detected ferromagnetic occurrences overlaid - developed jointly with the companion Energetic Horizon sensing module.

SGEM 2026 · Albena, Bulgaria #COSMOBOSS06 / 16
AGHWNiG
AGH University of Krakow
Faculty of Drilling, Oil and Gas
#COSMOBOSS · Tracked Micro-Rover
Slide 06 · The first build

Prototype Tracks: Rubber Configuration

The prototype used rubber tracks of width 2 cm and length 16 cm; each track carries 68 grousers that increase effective contact area and total traction.

Grousers improve grip on loose soil and prevent loss of adhesion - vital for such a small vehicle, which on a flat surface under low gravity can easily slip. The prototype has a small mass of only 400 g; later versions, using heavier and more durable materials and more accurate instruments, will weigh several times more.

400 g
Mass
68
Grousers / track
2 cm
Track width
16 cm
Track length
0.0064 m²
Total contact area
SGEM 2026 · Albena, Bulgaria #COSMOBOSS07 / 16
◉ Interactive · gravity slider · live p = m·a / S
AGHWNiG
AGH University of Krakow
Faculty of Drilling, Oil and Gas
#COSMOBOSS · Tracked Micro-Rover
Slide 07 · Earth vs. Moon - live

Ground Pressure: Earth vs. Moon

p = m · a / S
m = 0.400 kgS = 0.0064 m²
a = 9.81 m/s²
Bodya [m/s²]p [Pa]
Earth9.81613.1
Moon1.62101.3

Live ground pressure

613.1Pa

Earth reference - full weight on the contact patch.

SGEM 2026 · Albena, Bulgaria #COSMOBOSS08 / 16
AGHWNiG
AGH University of Krakow
Faculty of Drilling, Oil and Gas
#COSMOBOSS · Tracked Micro-Rover
Slide 08 · The next iteration

Next Version: Segmented 3-D-Printed Tracks

Rubber tracks will be replaced by purpose-designed, 3-D-printed segmented tracks; each segment carries a grouser, a guide tooth, and a hinge connecting successive segments.

Six road wheels were adopted as the optimum number: per Hou et al. (2021), this limits the sinking of tracks into regolith by about 35% - highly important given the small ground clearance of low-slung micro-rovers.

Segmented-track configuration on Earth: m = 0.4 kg, n = 6 road wheels of d = 3 cm, pitch p_t = 2 cm, width b = 5 cm → single-road-wheel ground pressure ≈ 58.8 Pa.

Key design choices

  • 3-D-printed segmented track
  • Grouser + guide tooth per segment
  • 6 road wheels (optimum) → ~35% sinkage reduction
58.8 Pa
Single road-wheel p (Earth)
~35%
Sinkage reduction
SGEM 2026 · Albena, Bulgaria #COSMOBOSS09 / 16
AGHWNiG
AGH University of Krakow
Faculty of Drilling, Oil and Gas
#COSMOBOSS · Tracked Micro-Rover
Slide 09 · Experimental setup

Test Stand and Methodology

A 60 × 100 cm field holds a ~10 cm layer of the lunar regolith analogue AGK-2010, with bauxite blocks as obstacles; a camera recording at 60 fps is mounted on a tripod spanning the whole stand.

AGK-2010 is a Polish analogue of the CHENOBI simulant, with comparable grain-size fraction and internal friction angle, and a bulk density of 1.295 kg/l (about 1.45% below CHENOBI). A characterised analogue is essential: grain-size distribution, density, cohesion and internal friction angle govern traction and sinkage.

Test-stand parameters

  • Field 60 × 100 cm, regolith depth ~10 cm
  • Analogue AGK-2010 (CHENOBI-class)
  • Bulk density 1.295 kg/l (−1.45% vs CHENOBI)
  • Bauxite obstacle blocks
  • Camera 60 fps, full-span tripod
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AGHWNiG
AGH University of Krakow
Faculty of Drilling, Oil and Gas
#COSMOBOSS · Tracked Micro-Rover
Slide 10 · Defining the index

Control Test and Speed-Loss Index

In the control run the tracks are lifted clear of any surface and motors run to maximum speed in air (no friction load). No-load speed: V₀ = L / t, with L = 0.4 m total track length.

Mean revolution time t = 0.45 s → no-load maximum speed V₀ ≈ 0.89 m/s. In the research test the rover crosses the regolith field, and the dimensionless speed-loss index is evaluated as a trafficability proxy - not a Coulomb friction or traction coefficient.

The speed-loss index

μ = (V₀ − Vk) / (g · Δt)
  • V₀ = no-load max speed
  • Vk = max speed on regolith
  • g = 9.81 m/s²
  • Δt = acceleration time
0.89 m/s
Control V₀
0.45 s
Mean rev. time t
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◉ Interactive · hover bars · animate runs
AGHWNiG
AGH University of Krakow
Faculty of Drilling, Oil and Gas
#COSMOBOSS · Tracked Micro-Rover
Slide 11 · Seven runs on AGK-2010

Mobility Results: Seven Runs

RunVk [m/s]Δt [s]μ [-]
10.450.670.0403
20.580.520.0690
30.510.590.0636
40.580.520.0678
50.470.640.0636
60.560.540.0689
70.380.780.0652
Mean0.500.610.063

Speed-loss index μ per run

Hover a bar - dashed line = mean μ̄ ≈ 0.063
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AGHWNiG
AGH University of Krakow
Faculty of Drilling, Oil and Gas
#COSMOBOSS · Tracked Micro-Rover
Slide 12 · Interpreting the results

Discussion: What μ̄ ≈ 0.063 Means

The mean speed-loss index μ̄ ≈ 0.063 (runs 0.040-0.069) means the rover reaches roughly 50-65% of its no-load top speed on the analogue - loose soil resists motion only weakly, favourable for trafficability.

This index is a motion-resistance proxy, not a friction or traction coefficient. The internal friction angle of regolith simulants is φ ≈ 31-50°, and the drawbar-pull coefficient of grousered tracks on soft soil is typically 0.4-0.7 - an order of magnitude larger and of different physical origin.

Read it carefully

  • μ̄ ≈ 0.063 → reaches 50-65% of no-load speed
  • Proxy for motion resistance, not friction
  • φ of simulants 31-50°
  • Drawbar-pull coeff. 0.4-0.7 (×10 larger)
  • Scatter 0.040-0.069, run 1 a low outlier

Proper traction characterisation via drawbar-pull and slip measurements is required before any design coefficient is quoted.

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AGHWNiG
AGH University of Krakow
Faculty of Drilling, Oil and Gas
#COSMOBOSS · Tracked Micro-Rover
Slide 13 · Honest boundaries

Limitations

① Gravity itself

Both control and research tests are on Earth, yet traction and the mechanical response of regolith change under reduced gravity - reduced-gravity experiments report measurable loss of traction and increased relative sinkage as gravity decreases. Terrestrial figures are conservative references, not direct lunar predictions. Faithful prediction needs reduced-gravity testing (parabolic flight, counterweight rigs) or validated terramechanics scaling.

② The cost-mass trade-off

The historical cost-mass trade-off excluded tracks from planetary missions. This work reframes rather than removes it: for drilling-capable micro-rovers, the mass that makes tracks expensive is the same mass that makes drilling possible.

SGEM 2026 · Albena, Bulgaria #COSMOBOSS14 / 16
AGHWNiG
AGH University of Krakow
Faculty of Drilling, Oil and Gas
#COSMOBOSS · Tracked Micro-Rover
Slide 14 · Synthesis

Conclusion

The paper presented the concept and prototype of the tracked #COSMOBOSS micro-rover - a palm-class platform departing from the wheeled convention of planetary rovers in order to carry a drill.

The central rationale - turning the historical drawback of tracks (their mass) into the principal advantage for a drilling micro-rover - is supported by a reproducible mobility-testing methodology and seven runs giving a low mean speed-loss index of about 0.063, confirming good trafficability on AGK-2010.

Take-home points

  • Mass: drawback → principal advantage for drilling
  • Reproducible mobility-testing methodology
  • 7 runs, mean μ̄ ≈ 0.063 → good trafficability
  • Proposed segmented 3-D-printed track: grousers + guide teeth + 6 road wheels
  • Satisfies mass & low-ground-pressure requirements simultaneously
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AGHWNiG
AGH University of Krakow
Faculty of Drilling, Oil and Gas
#COSMOBOSS · Tracked Micro-Rover
Slide 15 · The road ahead

Future Work

  • (i) Replace the provisional motion-resistance index with proper traction characterisation from drawbar-pull and slip measurements; extend the dataset, add sinkage measurements; benchmark AGK-2010 against standard simulants.
  • (ii) Validate the six-road-wheel sinkage prediction experimentally.
  • (iii) Extend tests towards reduced-gravity conditions to correct the terrestrial results.
  • (iv) Integrate a drilling payload to demonstrate the weight-on-bit benefit in practice - connecting locomotion work directly to the Club's broader lunar drilling and ISRU programme.
Thank you

Questions welcome · SGEM 2026, Albena

AGH University of Krakow · Faculty of Drilling, Oil and Gas · #COSMOBOSS

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COSMODRILL · Scientific Club

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