Rolladen-Schneider LS4

LS4
Role Club-class (previously Standard-class) sailplane
National origin Germany
Manufacturer Rolladen-Schneider
First flight 1980
Number built 1,048


The Rolladen-Schneider LS4 is a Standard Class single seat glider manufactured by Rolladen-Schneider Flugzeugbau GmbH between 1980 and 2003.

Development

The LS4, successor to the LS1 in the Standard Class, made its first flight in 1980. It is the fourth most produced non-military glider (after the Grunau Baby, Blaník, and Schleicher K 8 trainers). A total of 1,048 were built until Rolladen-Schneider entered receivership in 2003. Its long production run is comparable only to that of the Schempp-Hirth Discus.

The LS4 won the first two places in the Standard Class at the 1981 World Championships in Paderborn, West Germany, and the first six places (and twenty-one out of the first twenty-five) at the 1983 Worlds in Hobbs, New Mexico. It is still a favourite in handicapped competitions and as a club and recreational aircraft.

This type consolidated Rolladen-Schneider's reputation for well rounded sailplanes that are both easy to fly and top performers. It is docile enough for beginners and its performance is only slightly below the latest standard class sailplanes. Given the continued interest in the type, the LS4 may be put back in production by the Slovenian manufacturer AMS-Flight.

The LS4 was succeeded by the LS7.

Design

The design of the LS4 was influenced mainly by the experience Rolladen-Schneider had gained with the LS2 and LS3 flapped gliders. Wolf Lemke returned to a double-tapered wing planform, giving it a larger area comparatively to the LS1 and LS2, and enlarged all control surfaces: the ailerons were elongated and brought further inboard and the tailplane span was increased.

The fuselage and vertical stabilizer were taken from the LS3 moulds. Other notable features of the design were the retractable landing gear, the centre of gravity tow release that retracts with landing gear, the heel-operated wheel brakes, the upper wing surface air brakes and the water ballast system with internal bags.

Structure

The structure is entirely glass-reinforced plastic mostly with synthetic foam cores. The exterior coating, as with most composite gliders, is gelcoat, which protects the load-bearing composite from humidity and UV-radiation, and is thick enough to allow wing profiling, which is done by hand during the finishing stages of manufacturing to achieve the smoothness required for extensive laminar flow.

Variants

LS4
The initial production version
LS4-a
featured larger water ballast bags allowing for an additional 15 l (3.96 US gal; 3.30 imp gal) of water to be carried in each wing. The landing gear system is strengthened by the addition of one extra set of shock absorption bumpers in order to handle the increased gross weight with a full water ballast load.[1]
LS4-b
fin height increased by 0.11 m (4.3 in) to 1.43 m (4 ft 8 in). The -b fuselage is 0.13 m (5.1 in) shorter at 6.66 m (21.9 ft). The wing shells are made in carbon, control connections are automatic, the instrument panel tilts up with the canopy and it has an optional tail fin water ballast system.

Specifications (LS4)

Data from Jane's All the World's Aircraft 1988-89[1]

General characteristics

LS4-a: 240 kg (530 lb)
LS4-a: 525 kg (1,157 lb)
LS4-a: 160–170 l (42–45 US gal; 35–37 imp gal)

Performance

180 km/h (97 kn; 110 mph) in rough air
180 km/h (97 kn; 110 mph) on aero-tow
130 km/h (70 kn; 81 mph) on winch launch
LS4-a280 km/h (150 kn; 170 mph) in smooth air
LS4-a190 km/h (100 kn; 120 mph) in rough air
LS4-a190 km/h (100 kn; 120 mph) on aero-tow
LS4-a140 km/h (76 kn; 87 mph) on winch launch
LS4-a: 50 kg/m2 (10.24 lb/sq ft)

See also

Aircraft of comparable role, configuration and era
Related lists

References

  1. ↑ 1.0 1.1 John W.R. Taylor, ed. (1988). Jane's All the World's Aircraft 1988-89. London: Jane's Information Group. p. 628. ISBN 0-7106-0867-5.

Further reading

External links

Media related to LS4 at Wikimedia Commons