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Terramechanics and off-road mobility

Maximum climbable grade

The steepest slope a vehicle can climb at steady speed on firm ground with a given available thrust, for small angles.

Ref
TER-03
Rev
v1
Field
Terramechanics and off-road mobility
Result
Gmax [%]

H is the thrust available at the ground, m the vehicle mass and Crr the rolling resistance coefficient. For steady climbing without towing, H = m g (sin θ + Crr cos θ). For small slopes sin θ ≈ tan θ and cos θ ≈ 1, giving tan θ ≈ H / (m g) − Crr, and the result is the grade 100 tan θ in per cent. At steep slopes the approximation slightly underestimates the grade. The thrust must be less than the grip limit, and a negative result means the thrust does not even overcome rolling resistance on level ground.

The steepest slope a vehicle can climb at steady speed on firm ground with a given available thrust, for small angles. It is the thrust-to-weight ratio less the rolling resistance coefficient.

Calculator

Solve for
%
kN
5100
kg
2,00060,000
0.010.3
  • Thrust-to-weight ratio, H / m g25.48 %
  • Slope angle for this grade, tan⁻¹(G / 100)12.13 °
  • Grade from the exact balance sin θ + Crr cos θ = H / m g22.1 %

What drives the result

Each variable is moved across its typical range while the others stay at the values above. The longest bar is the key driver.

Maximum grade (%) current value 21.48 %
mVehicle massKey driver
0.247123
HAvailable tractive thrust
1.197.9
CrrRolling resistance coefficient
−4.5224.5
  • With 25 kN of thrust on a 10 t vehicle (a thrust-to-weight ratio of 25.5 %) and Crr = 0.04, the steepest grade is 21.48 %. The exact balance gives 22.1 %, so the small-angle formula is slightly conservative.
  • On soft ground the loss is large: with Crr = 0.15 the limit falls to 10.48 %, and traction, not thrust, usually decides first (see the slope traction limit).
Chart data as tables

Ranked variables

VariableTypical rangeLowest resultHighest resultSwing (%)Local stepChange in result
m Vehicle mass2,000 to 60,000 kg0.2474123.4123.2+10%−10.8 %
H Available tractive thrust5 to 100 kN1.09797.9496.84+10%+11.9 %
Crr Rolling resistance coefficient0.01 to 0.3 −4.51624.4829+10%−1.86 %

Sweep of Available tractive thrust

Available tractive thrust (kN)Maximum grade (%)
51.097
16.8813.2
28.7525.31
40.6337.41
52.549.52
64.3861.62
76.2573.73
88.1385.83
10097.94

Sweep one variable

Maximum grade (%)Hover, touch, or use the arrow keys on the chart
020406080100 20406080100 Available tractive thrust (kN) now 21.48

Variables and how each one contributes

Gmax

Maximum grade

Result · %

What the equation gives you. Everything else feeds it.

H

Available tractive thrust

kN · typical 5 to 100

The tractive thrust available at the ground, in kN: the smaller of the engine force and the traction limit. Raises the grade in direct proportion to H / (m g), so the result responds more than in proportion, since the rolling term is subtracted. Raising it by 10 % (to 27.5) moves the result by +11.9 %, from 21.48 to 24.03 %.

m

Vehicle mass

kg · typical 2,000 to 60,000

The vehicle mass, in kg. Lowers the thrust-to-weight ratio and so the grade the vehicle can climb. Raising it by 10 % (to 11,000) moves the result by −10.8 %, from 21.48 to 19.17 %.

Crr

Rolling resistance coefficient

· typical 0.01 to 0.3

The rolling resistance coefficient of the surface. Subtracts directly from the thrust-to-weight ratio. A soft surface costs a lot of climbing ability. Raising it by 10 % (to 0.044) moves the result by −1.86 %, from 21.48 to 21.08 %.

Worked example with the values above

  1. Thrust-to-weight ratio: H / (m g) = 25,000 / (10,000 × 9.81) = 0.2548.
  2. Subtract the rolling coefficient: tan θ ≈ 0.2548 − 0.04 = 0.2148.
  3. Grade = 100 × 0.2148 = 21.48 %.

Assumptions and limits

  • Steady speed, no towing, no aerodynamic drag, and the thrust fully available (not grip limited).
  • A small-angle approximation, valid below about 25 to 30 % grade, and a constant rolling coefficient.

Common mistakes

  • Using the engine force at the tyre without checking that the tyres can transmit it.
  • Reading the result as a slope angle in degrees. It is a grade in per cent.

Statistics and uncertainty

The grade is a difference of the thrust-to-weight ratio (known to ±5 to 10 %) and the rolling coefficient (±30 %), so for a modest thrust margin the error is large: at the defaults a 10 % error in H shifts the grade by about 2.5 percentage points. The small-angle formula adds a systematic error of about 3 % of the grade at 20 %. Test climbs on the actual surface are the only reliable rating.

Where it is used

  • Gradeability ratings for military, agricultural and off-road vehicles.
  • Checking if a vehicle can meet a required slope, or how much a load reduces it.

Maths you need

  • Thrust-to-weight ratio: force divided by weight
  • Grade and slope angle: grade % = 100 tan θ

Related formulas

Practise this formula