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47-509: By the mid–to–late eighties the LS4 had lost its leading position in the Standard Class to new arrivals, in particular the excellent Discus from Schempp-Hirth . The LS7 , in spite of its advanced design, did not recapture the lead and, with flagging sales, Rolladen-Schneider went back to the drawing board. Designer Wolf Lemke was skeptical of the usefulness of developing a new airfoil. There

94-526: A feature of all World and European Championships. Technological development has eroded the performance gap that once existed between the Standard and 15-metre classes, which today is perceptible only in strong gliding weather. Some observers argue that the difference is not meaningful enough, that the 18 metre class is the natural successor to the 15 metre class and that the latter should be removed from World Championships to give space to new classes. Notwithstanding,

141-516: 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,

188-588: A low-cost sailplane, which should have moderate performance, be easy to assemble and to handle, and safe for inexperienced pilots to fly. The idea behind the project was to make gliding competitions more affordable and popular. The winning design was announced in 1993 as the Warsaw Polytechnic PW-5 , thus becoming the only glider allowed to take part in the competition. The first World Class World Championship took place in 1997 in Inonu , Turkey , but participation

235-686: A major fraction of the drag of sleek fibreglass airframes. Designers reacted by recessing the wheels into the fuselage, which further increased the risk of ground-related damage. Manufacturers took to arguing that the single cheapest way to increase performance was to retract the wheel. In view of these safety and cost-related arguments, the Standard Class rules were updated to allow disposable water ballast and retractable undercarriages. Retractable wheels were allowed by 1970 and water ballast by 1972. Manufacturers were fitting these as production items, and they had to be disabled to fly in competitions. In 1965

282-542: A modern Two Seater Class with a span limitation of 20 metres and maximum all-up weight of 800 kg. This class has no relationship to the 'old' two-seater class, as it targets the high performance trainers that have been steadily gaining in popularity. Their smaller size sets them apart from the Open Class two-seaters which are very expensive and require experienced crews. The 20 metre two-seaters handle and fly more like Standard Class single-seaters and cost little more than half

329-559: A prototype mainly due to the use of unidirectional carbon fibre on the wing skins, an attempt by Rolladen Schneider to improve the surface finish. Production turbos returned to using woven carbon again because of the increased production costs associated with using the more difficult to cut and handle unidirectional material. The LS8 is a flexible and relatively conservative design with high development potential. Although primarily designed to Standard Class specifications, it has lent itself easily to span extensions, motorisation, etc. Following

376-482: A ‘turbo’ or sustainer version were developed. A total of 491 examples of all subtypes had been manufactured by December 2005. Despite the commercial success of the LS8 the company producing it failed to prosper and after a slightly acrimonious court battle the LS8 and other Rolladen-Schneider aircraft passed to DG (DG Flugzeugbau) where it is still currently in series production. The LS8 manufactured by DG has some alterations to

423-513: Is a significant factor in the decline of the World Class, as it is equally affordable, yields higher performances and allows a degree of personal choice in equipment that does not exist in the World Class. The International Gliding Commission (IGC/CIVV) which is part of the FAI and an associated body called Organisation Scientifique et Technique du Vol à Voile (OSTIV) announced a competition in 1989 for

470-613: 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 . 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

517-527: Is the Ka 6 . Technological change was fast-paced in the years following the introduction of the Standard Class. The transition to fibreglass construction made the existing rules increasingly awkward. The stronger composite structures allowed higher wing loadings, and competitors resorted to fixed ballast to exploit this competitive advantage, which of course increased landing speeds and the risk of damage when alighting in unprepared fields. The fixed undercarriages caused

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564-670: Is the fifth most produced non-military glider (after the Grunau Baby , Blaník , Schleicher K 8 trainers and Grob G102 Astir .) 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 Grob G102 Astir and 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

611-401: Is the sporting body overseeing air sports at the international level so that essentially the same classes and class definitions are followed in all countries. Seven glider classes are currently recognised by the FAI and are eligible for European and World Championships : Gliding World Records are classified by the FAI under sub-classes that do not have a one-to-one correspondence with

658-461: Is understood to exclude the current state-of-the-art gliders. Water ballast is not permitted. The class is perceived as being fair in spite of the differences in glider performance. This may become compromised by the trend towards modification/customisation of Club Class gliders in ways that distort the handicapping and are difficult to control by the sporting bodies. The emergence of the Club Class

705-475: The ASW 22 and Nimbus-3 were introduced in 1981, after which the Open Class for a while became the exclusive preserve of only two manufacturers. The World Gliding Championships of 2012 brought into competition new designs, some of significantly lower wingspan, which flew successfully against "traditional" (wingspan 28 m+) machines of this class. Following a couple of decades of small, incremental performance gains,

752-589: The Akaflieg Darmstadt D-30 of 1938, which had variable-dihedral wings and spars built of light alloys, the extremely large-span SB-10 of 1972, the telescoping-wing Akaflieg Stuttgart FS-29 of 1975 and the solar-powered Icare . In contests, the Open Class usually delivers the top performances, with daily tasks as far as 1000 km being possible in favourable weather. To be successful, however, an Open Class glider must blend high performance with practicality. "Extreme" designs tend to be failures, of which

799-615: The Austria of 1931, the Sigma of 1971 and the BJ series are but the most conspicuous examples. Arguably the only 'extreme' glider that ever won a World Championships was the Nimbus I . Until the 1960s, a fair number of gliders were able to do well in open competition, with smaller-span types occasionally beating larger but more cumbersome types. The composite revolution caused a shake-down, further aggravated when

846-664: The 15 and 18 metre classes with interchangeable wing tips: the AS 33 (2020), the Ventus-3 (2016), and the JS-3 (2017). A two-seater class appeared for the first time in a World Championships in 1952. The reason for having a separate class was that the drag of the larger fuselage put two-seaters at a significant disadvantage vis-à-vis single seaters. This class was discontinued after the 1956 World Championships, although two-seater World records were retained until 1996. The IGC voted in 2005 to reinstate

893-588: The 1997 World Gliding Championships at St Auban, France; six out of the first ten positions in the 1999 World Gliding Championships in Bayreuth, Germany; the first three places in the 2001 Women's World Gliding Championships in Lithuania and, more recently, first (and nine out of the first ten places) in the 2005 Women's World Gliding Championships in Klix, Germany. In 2006 World Gliding Championships at Eskilstulna, Sweden, LS8 took

940-573: The American Richard Schreder flew a variant of his HP-11 , which in normal form had simple flaps as airbrakes. To comply with the rules, the ship was modified for the World Championships so that the outer half of the flaps hinged upwards to comply with the rules. Schreder pointed out that this made the glider more expensive and less safe (higher landing speed, less effective brakes). The argument over whether to allow this went on for

987-502: The Formula 1 industry. The prop which extended rapidly through a pneumatic mechanism was belt driven via a belt that ran inside the pylons which were Carbon Fibre aerofoil sections to minimise drag. The engine could be started using a starter motor before deploying the prop with the engine already running, a small alternator then recharged the battery and pneumatic reservoir. Air inlet and exhaust were accomplished through small pneumatic doors it

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1034-479: The German Championships at Neustadt-Glewe. The LS8 that finally emerged in 1994 had a few improvements over the prototype, the most significant being the redesigned ailerons and the lighter and aerodynamically cleaner wing made possible by deleting the flap system. Examples of the LS8 scored second, fourth and fifth in the 1995 World Gliding Championships at Omarama, New Zealand; first, second and third in

1081-561: The Standard and 15 metre classes. Some significant Standard Class types have been the Ka 6 and Mucha (1958), the LS1 (1967), the Standard Cirrus (1969), the LS4 (1980) and the Discus (1984). Modern contenders include the Discus 2 (1998), LS8 (1995) and ASW 28 (2000) This class was created specifically to end the trailing-edge airbrake controversy in the Standard Class. The class has been very successful, being since its inception

1128-479: The above competition classes: Glider classes not recognised by the FAI have been used in some regional and national competitions. The most significant of these are: The Open Class is the oldest competition class, although it only came into formal existence with the creation of the two-seater class in the early 1950s. This unrestricted class has been a favourite testing ground for technological innovation. Many research prototypes fall under this class definition, e.g.

1175-516: The appearance and performance of shorter wingspan competitors in World Gliding Championships of 2012 may change established views on the design trends. In July 2007, the IGC increased the maximum weight allowed in the Open Class to 850 kg provided the aircraft has a valid certificate of airworthiness at that weight, i.e. the manufacturers must re-certify the glider. The Standard Class

1222-500: The appearance in 2000 of the eta brought a sudden jump in performance and a further price escalation. This very expensive aircraft has up to now not had outstanding success in competition, but it for a while seemed to impact the cost of remaining competitive in the class. The 'eta biter' and its successor, the Concordia single-seater, as well as Walter Binder's EB28 / EB29 until 2012 were being presented as challengers to eta, but

1269-544: The bottom of the fuselage again to allow engine running with the prop/pylons still in the bay and the main fuselage doors still closed. This arrangement whilst being greatly admired by many was determined by the manufacturer to be too complex and expensive and a much more conventional Turbo design was eventually selected for production by Rolladen Schneider. The LS design has since been modified by DG after their acquisition of LS (Rolladen-Schneider) with DG's in house DEI NT engine control system. The original Prototype LS8-t (Turbo)

1316-506: The class and created a parallel 15 metre Class to accommodate them. This decision was polemic as it was the second rule change in a few years and it orphaned several glider types that did not fit well within either class definition (especially the PIK-20 and the Libelle that had been built in large numbers). Notwithstanding, the decision was vindicated by the great success subsequently enjoyed by both

1363-649: The class has a sizeable following and official support into the foreseeable future. Significant 15 metre types include the ASW 20 (1977), Ventus (1980), LS6 (1983). Modern contenders include the Ventus-2 (1994), the ASW-27 (1995) and Diana 2 (2005). The availability of carbon fibre at affordable prices has allowed the manufacture of light and economical spans exceeding 15 metres. Manufacturers started to exploit this potential by offering tip extensions for their flapped sailplanes. Spans increased gradually from 16.6 metres in

1410-411: The demarcation line between airbrake/landing flaps and performance enhancing flaps is vague. The reluctance within the IGC to allow the later in the Standard Class led to an unsuccessful attempt to codify what constitutes a landing flap. After the LS2 and the PIK-20 exploited this loophole to win the 1974 and 1976 World Championships in the Standard Class, the IGC banned all camber-changing devices from

1457-417: The first and third places. LS8 was the winner of 2002, 2004, 2005, and 2007 European Gliding Championship. Many regard it as the best all-round standard class glider. Commercially the LS8 was very successful, due to its competition potential and to the gentle and easy flight characteristics that make it suitable for club and leisure flying. Primarily to cater to the latter market, versions with longer wings and

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1504-445: The first implementations ( ASW 20L and Ventus b 16.6 ) to 17 metres ( DG-200/17 , DG-600 , Glasflügel 403 ), 17.5 metres ( LS6-c ), finally settling on 18 metres. The trend towards turbo and self-launching sailplanes also favours the 18 metre span, which is large enough to carry the additional weight of the power unit without impairing the ability to climb in weak lift. Following a decade of contests at regional level, which permitted

1551-448: The first six places (and twenty-one out of the first twenty-five) at the 1983 World Championships 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

1598-497: The mainwheel, the Turbo version etc., and slightly different model designations from the originals. The development of the sustainer "Turbo" version went through several iterations with the original prototype being manufactured by Rolladen Scheider for Peter Wright who designed a unique turbo design where the engine remained in the engine bay and drove the propeller via a belt. Peter had many years experience working in composites, design and

1645-428: The next five years in IGC and eventually the rules were changed to permit plain flaps provided they were the only means of drag control for landing, and there was no aileron linking for camber changing. There were no other limits on using the flaps for lift increase (although the lack of aileron linking meant that the flaps were not as effective as they might have been). A later concession would bring difficulties in that

1692-415: The number of entrants is not large enough to warrant their separation into the usual classes. The formal recognition by the FAI of a handicapped class is quite recent, with the first Club Class World Championships having taken place in 2001. It is intended by the FAI as an affordable entry-level class. It has been extremely successful, attracting some of the most talented and experienced pilots in addition to

1739-582: The price of an Open Class glider. Gliders in this class include the Duo Discus (unflapped), Arcus (flapped), ASG 32 , and the DG-1000 , with the older Janus and DG-500 also being eligible. Handicapped contests have been a long-standing feature of many regional and national level events. These Club or sports contests allow the use of gliders of widely differing levels of performance. They are thus popular in places where mostly older types are available, or where

1786-522: The resolution of issues such as mixed glider/motorglider competition, this class came to feature for the first time in a World Championships in 2001, with a maximum all-up weight of 600 kg. Significant 18 metre types include the Schleicher ASG 29 (2005), Schempp-Hirth Ventus-2 (1995), and the Jonker JS-1 (2007). The same three manufacturers have since introduced new types which are competitive in both

1833-594: The smoothness required for extensive laminar flow . Data from Jane's All the World's Aircraft 1988-89 General characteristics Performance Aircraft of comparable role, configuration, and era Related lists FAI Standard Class Competition classes in gliding , as in other sports, mainly exist to ensure fairness in competition. However the classes have not been targeted at fostering technological development as in other sports. Instead classes have arisen because of: The FAI Gliding Commission (IGC)

1880-428: The transfer of ownership, subtype designations and specifications changed slightly. General characteristics Performance Related lists Rolladen-Schneider LS4 The Rolladen-Schneider LS4 is a Standard Class single seat glider manufactured by Rolladen-Schneider Flugzeugbau GmbH between 1980 and 2003. The LS4, successor to the LS1 in the Standard Class , made its first flight in 1980. It

1927-436: The upper wing surface air brakes and the water ballast system with internal bags. 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

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1974-430: The young and impecunious. Among the reasons for this are the long lifespans of gliders that invite their continued use, the relative simplicity of the class rules and the typically more relaxed "atmosphere" of Club Class competitions. The glider types allowed are not explicitly defined. The criterion for admission is given by an interval of performance handicaps which may be adjusted by the organisers of each event but that

2021-642: Was (after difficulties with new EASA regulations trying to export the aircraft to France) converted back to a more or less standard LS8-b where it remains on the British BGA register now redesignated as the LS8-PW (so named after Peter Wright who designed and built the engine installation) with the Competition number F1. It is still unique in being the only LS8 currently on the CAA EASA Annex II list due to its status as

2068-504: Was however achieving surprisingly good results flying with locked flaps in the non- FAI sanctioned Sports Class in the United States. Following this lead, Rolladen-Schneider modified an LS6-c by removing the flap handle, resetting the wing at a slightly higher angle of incidence and adding winglets. This experimental prototype outperformed state-of-the-art standard class sailplanes both in side-by-side flight tests and in contests including

2115-407: Was introduced in the late fifties as an alternative to the increasingly heavy, difficult to fly and costly Open Class ships of that time. Striving for affordability and simplicity, the original standard class rules restricted the span to 15 metres and ruled out retractable undercarriages, flight-disposable ballast, radios and lift-enhancing devices such as flaps. The archetypal embodiment of these rules

2162-401: Was no guarantee that the large effort and investment required would bring any palpable gains, as the LS7 , ASW 24 and DG-600 had clearly shown. The tools available at the time were simply not up to the task of reliably predicting the performance in everyday conditions of the newer laminar-flow profiles then emerging from the research labs. The 15–meter Class LS6 , which first flew in 1983,

2209-580: Was not as high as has been expected. World Class world championships have ceased after 1 October 2014. This class will be replaced by a 13.5 metre Class in which more types of gliders with disposable ballast will be permitted. First World gliding championship of the 13.5 metre Class took place in August 2015 in Lithuania. A glider with a take-off mass not exceeding 220 kg is in the DU Ultralight Class. This class has been defined for world records but there

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