STATIC WEIGHT
Dynamic loads in offshore lifting

When the sea moves, the hook load climbs above the static weight.

Dynamic Amplification Factor (DAF)

What is Dynamic Amplification Factor?

The Dynamic Amplification Factor (DAF) is the ratio of the maximum dynamic load to the static load during a lifting operation. A DAF of 1.0 means no dynamic effect — the crane sees only the static weight of the payload. A DAF of 2.0 means the peak dynamic load is twice the static weight.

Practical application: For practical application of this topic, see POLARIS crane shock absorber and engineering studies and analysis.

In offshore lifting, waves cause the crane tip to move up and down while the payload hangs below. This relative motion creates dynamic forces in the lifting system — tension spikes when the crane tip accelerates upward, and slack when it drops. The DAF captures how much worse these dynamic forces are compared to a calm-water lift.

Typical DAF values for offshore lifts without compensation range from 1.2 to 2.5, depending on sea state, crane stiffness, and sling length. With a heave compensator installed, the DAF can be reduced to 1.05–1.3, which means smaller cranes can lift the same payload or the same crane can operate in rougher seas.

What causes DAF in real crane lifts?

In real crane lifts, DAF is usually caused by relative motion. The crane tip, hook, wire, slings and payload do not all move together. When the system suddenly takes up that motion, the wire and rigging behave like springs and the velocity difference becomes a tension spike.

Supply-vessel deck lift. A cargo container on a supply vessel follows the vessel heave and roll, while the crane tip follows the crane vessel or platform. If the hook is moving up as the deck or container is moving down, the sling can go from slack or low tension to fully loaded in a fraction of a second. This snap load can be much higher than the static container weight.

Splash-zone crossing. During a splash-zone crossing, buoyancy, drag, added mass and wave particle velocity change quickly as the payload passes through the free surface. The hook load can rise and fall rapidly, especially when the crane, wire and payload dynamics line up with the wave period.

Other common triggers include sudden lift-off from deck, landing impact, snagging, fast crane motion, emergency stops and resonance in the crane-wire-payload system.

Snap loads — the worst-case DAF

The most violent DAF events are snap loads: the sling goes slack, then re-tensions suddenly. While the wire is slack the hook and payload move independently, and when it comes taut the velocity difference has to be absorbed by wire stretch almost instantly. For a payload of mass m (plus added mass mA if submerged) on rigging of stiffness k, the tension spike above the quasi-static load is approximately

F_{\text{snap}} = v_{\text{rel}} \sqrt{k \, (m + m_A)}

where vrel is the relative velocity at the moment the wire re-tensions. Both design handles are visible in the formula: reduce the velocity mismatch (slower crane motion, heave compensation systems, better weather) or reduce the effective stiffness k (a POLARIS crane shock absorber). Stiff rigging is the enemy here — doubling k raises the snap force by 41% for the same velocity mismatch. DNV-RP-N103 sets the criteria for when snap loads must be assessed and how the peak is calculated; the practical mitigation it points to is keeping the wire under tension through the whole wave cycle, which is exactly what a passive heave compensator does.

Simulated hook load at deck lift-off: bare rigging snaps to 3.2 times static load with repeated slack windows; a preloaded shock absorber holds the load near 1.3 times static
Figure 2 — Snap load at deck lift-off, illustrative 1-DOF simulation: 20 t payload, 4 MN/m hoist stiffness, 1.5 m/s relative velocity at engagement, crane tip heaving ζ = 1.0 m, T = 7 s. Bare rigging (navy) sees a 3.2× spike and repeated slack–snap cycles; a preloaded gas-spring shock absorber with damping (red) takes the same lift-off at 1.28× static. Illustrative model, not a certified calculation.

How to reduce DAF

  • Shock absorbers for snap loads. A POLARIS crane shock absorber adds stroke and damping between the crane and payload. It absorbs the kinetic energy of a single shock event — deck lift-off, a snap load, an overload — before it becomes peak crane load. It needs time to reset after an event, so for repeated slack–snap cycles in the wave zone, use heave compensation instead.
  • Passive heave compensation for splash-zone crossings. A passive heave compensator reduces relative motion between the crane hook and subsea payload. This keeps rigging tension smoother through the splash zone and reduces the dynamic amplification the crane sees.
  • Choose the compensator by operation. RIGEL and CYGNUS cover simpler passive cases, while ANTARES is used for complicated or multi-step subsea lifts with changing buoyancy.
  • Control the lift as well as the equipment. Lower crane speed, avoid resonant sea states, plan weather windows and use soft lift-off procedures. The equipment reduces DAF, but the operation still sets the starting conditions.

For product choice, start with the heave compensator selection guide or compare the crane demand in the crane load chart.

How to Calculate DAF

The simplest DAF estimate comes from DNV-OS-H205 (now DNV-ST-N001), which gives:

DAF=1+aheaveg

where aheave is the maximum vertical acceleration at the crane tip and g is gravitational acceleration (9.81 m/s²). For a sinusoidal heave motion with amplitude ζ and period T:

aheave=ζ×(2πT)2

For example, with a 1.5 m heave amplitude and an 8 s period:

aheave=1.5×(2π8)2=0.93m/s²DAF=1+0.939.81=1.09

This is the crane-tip DAF only — the hook DAF is usually higher because the sling and payload form a spring-mass system that amplifies the crane tip motion, especially near resonance.

Crane-tip DAF versus wave period for heave amplitudes 0.5 to 2.0 m: DAF rises steeply below 6 second periods; worked example at 1.5 m and 8 s gives DAF 1.09
Figure 1 — The crane-tip estimate DAF=1+ζ(2πT)2g across wave period. The (2π/T)² factor dominates — halving the period quadruples the dynamic part (DAF − 1): the same 1.5 m heave that gives DAF 1.09 at T = 8 s gives 1.38 at T = 4 s. In-air design values must also respect DNV-ST-N001’s weight-banded Table 16-1 minimums (offshore: 1.25 stepping down to 1.10 as hook load grows). Subsea lifts have no flat minimum — their DAF is calculated per Section 16.17 with RP-N103 methods, where a compensator directly lowers the result.

More accurate DAF calculations require modelling the full dynamic system: crane boom stiffness, wire rope elasticity, sheave friction, sling arrangement, and payload hydrodynamic properties. Tools like OrcaFlex are commonly used for this.

Typical DAF ranges

Lift scenarioUncompensatedWith compensationPrimary driver
General offshore lift1.2 – 2.51.05 – 1.3crane-tip heave & rigging stiffness
Subsea liftcalculatedcalculated — the compensator lowers it directlyST-N001 §16.17 with RP-N103 — no flat minimum; line tensions ≥ 10% of static
Snap / lift-off (worst case)up to ~3.2× (illustrative)~1.28× (shock absorber)slack-then-snap in the wire
Passive compensation pulls the DAF band down toward the static weight
General offshore lift · DAF range (× static weight)
1.0 static
UncompensatedWith passive compensation
Indicative ranges before design analysis; the design-basis DAF for a specific lift comes from a full analysis.

DAF by lift scenario

Offshore, DAF splits into two mitigation regimes — a repeated wave-cycle heave problem, and a single shock or snap event — and each has a different answer.

CONSTELLATION simulation of a passive heave compensator crossing the splash zone
Splash-zone crossing

Crossing the water surface

Entering the splash zone, slam, varying buoyancy and snap loads hit almost at once. Passive heave compensation keeps the sling taut and cuts the crane-motion part of the DAF; the water-entry slam itself stays a hydrodynamic (DNV-RP-N103) check.

Drivers: slam · varying buoyancy · crane-tip heave

CONSTELLATION simulation of a pile run with a crane shock absorber
Pile run & lowering

Running a pile or heavy structure

Lowering a long pile or heavy object at speed, a slack-then-snap or shock event at the crane tip drives the peak — a sharp, short-duration spike rather than a wave-cycle heave.

Drivers: snap / shock load · lowering speed · rigging stiffness

Cap the peak with — a crane shock absorber
One tool simulates both. CONSTELLATION models the splash-zone and pile-run dynamics — and the DAF — before the lift leaves the deck. Simulate your lift →

See the DAF, before the lift

Real CONSTELLATION runs for the two scenarios — the tension and load traces that show the DAF and how the equipment holds it.

CONSTELLATION tension-versus-time chart for a passive-compensated splash-zone lift, no slack no snap

Splash zone · RIGEL. Sling-group tension held through water entry — no slack, no snap. Payload DAF 1.10.

CONSTELLATION load-versus-time chart for a pile run with and without a crane shock absorber

Pile run · POLARIS. Peak crane-tip load with vs without the shock absorber — the spike capped in the run.

Estimate your DAF

1.22
estimated DAF

Crane-tip heave ζ ≈ 1.0 m; rigging amplification ≈ 3.5×. First-pass hook DAF — it captures crane-tip motion and rigging resonance (the DAF spikes when the wave period meets the rigging’s natural period Tn), but not splash-zone added mass, drag or slamming, so a snap-load peak can be higher still. For the design-basis DAF, commission a CONSTELLATION study.

Resonance: DAF spikes when the wave period meets your rigging
DAF vs wave period for your sea state & rigging · solid dot = your wave period · dashed line = the rigging’s natural period Tn
Crane-tip motion amplified by the rigging transmissibility: DAF=1+ζ(2πT)2g·TR — TR peaks when the wave period T meets the rigging’s natural period Tn.

DAF — frequently asked

What is a typical DAF for an offshore lift?
For a general offshore lift, DAF commonly falls between 1.2 and 2.5 uncompensated, and 1.05–1.3 with passive heave compensation. In-air lifts must respect the weight-banded Table 16-1 minimums of DNV-ST-N001 (offshore: 1.25 down to 1.10 as hook load grows); subsea lifts have no flat minimum — their DAF is calculated per Section 16.17 with RP-N103 methods. The design value for a specific lift comes from a full analysis.
How do you calculate DAF?
A first-pass crane-tip estimate is DAF=1+aheaveg, where aheave is the maximum vertical acceleration at the crane tip. It ignores rigging stiffness, added mass, drag and slamming, so a snap-load peak can be much higher.
What is a snap load?
A snap load is the impulsive spike when a wire goes slack and then suddenly re-tensions — the worst-case DAF driver, capable of reaching several times the static load in a pile-run or lift-off event.
How much does passive heave compensation reduce DAF?
By keeping the wire in tension and absorbing crane-tip motion, passive compensation typically brings a 1.2–2.5 DAF down toward 1.05–1.3 for splash-zone and subsea lifts.

DAF and Heave Compensator Selection

The primary engineering benefit of a heave compensator is DAF reduction. By decoupling the payload from the crane tip motion, the compensator absorbs the dynamic forces that would otherwise be transmitted through the lifting system.

A well-tuned passive heave compensator typically removes 70–95% of the dynamic amplification — the part of the hook load above the static weight — so a lift that would see DAF 2.0 without compensation (a 100% dynamic increase) drops into the 1.05–1.3 range with compensation. This has direct cost implications:

  • Smaller crane capacity needed for the same payload
  • Wider weather windows — lift in Hs 2.5 m instead of Hs 1.0 m
  • Reduced risk of sling overload and dropped objects
  • Lower dynamic loads on subsea structures during landing

For heavy subsea lifts where DAF control is critical, an adaptive passive compensator like ANTARES offers the best balance of DAF reduction and operational simplicity.

Related on Norwegian Dynamics

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