December 2025

IN THIS ISSUE. Training leaders for seagoing polar oceanography, cost-conscious measurements off Bangladesh, air-cushion travel for science missions in polar regions, ten pressing questions (and answers) about marine fungi, and more…

December 2025 | Oceanography

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tion of the camp site and environs (Figure 4). In each case, the

hovercraft was moved, instruments were recovered, and the oper-

ation was resumed after about three weeks. Total fuel consump-

tion during the 12 months of the 2,200 km long Fram-2014/15 ice

drift was equal to what an icebreaker burns in six hours of tran-

sit in heavy ice. For scale, an icebreaker transits from the ice edge

at 80°N north of Svalbard to the North Pole (1,100 km) in about

7–10 days under good ice conditions.

OPERATIONS IN ANTARCTICA

EARLIER USE OF HOVERCRAFT

Fuchs (1964) first proposed use of hovercraft for Antarctic travel,

and New Zealand made the first trial run using a small air cush-

ion pleasure craft in 1977 (Caffin, 1977). A more determined effort

was pioneered by Japanese scientists who built and started test-

ing an experimental hovercraft in 1981, followed by an Antarctic

evaluation period running until 1990 (Murao et  al., 1994). The

8 m long craft weighed 2.8 tons, had a 0.6 ton payload capacity,

and a hover height of 0.6 m. The activity was not pursued further,

as hovercraft technology was apparently not sufficiently mature at

this stage. Seven years later, two small hovercraft with payloads

of 300 kg were successfully used by the British Antarctic Survey

on the Larsen B Ice Shelf to tackle a surface littered with melt

puddles (James’ Hovercraft Site). During the 1988/89 season, the

US Antarctic Program operated a licensed-built Griffon TD1500

hovercraft in McMurdo. The 10 m long craft was powered by a

190 Hp engine, could take a 1.5 ton payload, and had a stated hover

height of 0.4 m. This craft operated on the Ross Ice Shelf and the

adjacent sea ice in McMurdo Sound in support of science pro-

grams. Cook (1989) summed up the positive experience (see also

https://www.southpolestation.com/trivia/history/hovercraft.html.

be passed. Pressure ridges are often several meters high but have

saddle points where a hover height as low as 0.5 m may be suffi-

cient for passage. Here is where the standard, narrow hovercraft

hull is an advantage. Hovercraft travel in the Transpolar Drift of

first year ice can be achieved with an efficiency not very different

from an icebreaker or transit on major highways on land between

the larger cities (Figure 3a, inset). The effective advance toward the

target may be 4–7 knots, varying with the abundance of obstruc-

tive pressure ridges (Kristoffersen and Hall, 2014).

The most critical issues for driving in sea ice are the light condi-

tions and terrain definition. The early spring from end of March to

mid-May have the best light conditions for aircraft and hovercraft

operations in the Arctic. As the summer progresses, low clouds

and diffuse light conditions (whiteout) become more prevalent,

and by mid-August the visibility sufficient for hovercraft driving

averages only a few hours per day (Kristoffersen and Hall, 2014).

Another consideration is the size of a hovercraft suitable

for operating in the sea ice environment. Our experience is

that a craft significantly larger (>11 m) and heavier (>7 tons)

than the Griffon TD2000 is likely to be less versatile—it does

not recover as easily from encounters with ice obstructions

(Kristoffersen and Hall, 2014).

HOVERCRAFT AS AN ICE DRIFT PLATFORM

There are several advantages to using a hovercraft as an ice drift

platform (Kristoffersen et  al., 2016). First, the mobility of the

accommodation and the instrument laboratory as one unit

directly translates into safety. Second, the need for manpower is

greatly reduced, making the hovercraft cost-effective to deploy.

For example, ice dynamics forced four camp relocations during

the Fram-2014/15 ice drift, two of which involved total destruc-

FIGURE 3. Overview of the hovercraft operations (red track lines) described

(a) in the Arctic Ocean and (b) in Antarctica. The inset shows a compari-

son of the efficiency of travel. Numbers for the track covered relative to

the great circle distance for the hovercraft and the icebreaker are for travel

between the ice edge and 85°N along 17°E in the Transpolar Drift. Numbers

for Ski-Doo and dog sled include travel in both the Beaufort Gyre and the

Transpolar Drift (Kristoffersen and Hall, 2014).

(a) Arctic Ocean

(b) Antarctica