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Schempp-Hirth Discus-2

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are an optional extra. A version with a narrow fuselage is called the Discus-2a and the wider fuselage version is called the 2b. The fuselage was specifically designed to be highly crash resistant. In U.S. Air Force service the Discus-2b is known as the
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A version with an 18-metre span, with the option of smaller wing tips to fly as a Standard Class glider, was launched in 2004 and designated Discus-2c. When fitted with a small sustaining engine (turbo) it is designated Discus-2cT.
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In plan view the almost crescent shape of the leading edge is similar to the Discus but is tapered in three stages. An entirely new
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has meant that the Discus-2 has not sold in such great numbers as its predecessor, which went unchallenged for many years.
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Production variant with 15 metre wingspan and narrow cockpit. 0.54 m (1.77 ft) in width, 0.75 m (2.46 ft) in height.
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Production variant with 15 metre wingspan and wider cockpit. 0.62 m (2.03 ft) in width, 0.81 m (2.66 ft) in height.
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200 kg (441 lb) water ballast, plus 7.8 kg (17 lb) in tail-unit tank
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Production variant with 15 metre or 18 metre wingspan equipped with a
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The Discus-2 has also been successful though the competition from the
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towards the tips was greatly increased compared with the Discus.
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Production variant with 15 metre or 18 metre wingspan.
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Aircraft of comparable role, configuration, and era
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Archived from 451:0.59 m/s (116 ft/min) 45:needs additional citations for 27:German single-seat glider, 1984 310:, 2 cylinder sustainer engine. 294:, 2 cylinder sustainer engine. 1: 728:Schempp-Hirth Discus-2 Series 18:Schempp-Hirth TG-15B Discus 2 1558:Aircraft first flown in 1997 413:525 kg (1,157 lb) 255:Alexander Schleicher ASW 28 1574: 406:242 kg (534 lb) 325:Specifications (Discus-2a) 1513: 966:designations 1962–present 139: 1361:1948 USAF redesignations 318:front electric sustainer 69:"Schempp-Hirth Discus-2" 1533:1990s German sailplanes 704:m-selig.ae.illinois.edu 533:16 October 2006 at the 515:16 October 2006 at the 339:General characteristics 1538:Schempp-Hirth aircraft 474:Rolladen-Schneider LS8 437:Max manoeuvring speed: 251:Rolladen-Schneider LS8 225:Design and development 204:Schempp-Hirth Discus-2 972:USAAC/USAAF sequences 1417:Tri-Service sequence 653:on 24 September 2015 443:Maximum glide ratio: 219:Schempp-Hirth Discus 54:improve this article 772:Wooden construction 411:Max takeoff weight: 152:General information 679:on 16 October 2006 428:Never exceed speed 1543:Electric aircraft 1520: 1519: 1356: 1355: 918: 917: 698:Lednicer, David. 644:Schempp-Hirth.com 479:Schleicher ASW 28 200: 199: 130: 129: 122: 104: 16:(Redirected from 1565: 1487: 978: 945: 938: 931: 922: 828:GRP construction 819:Standard Austria 757: 750: 743: 734: 715: 714: 712: 710: 695: 689: 688: 686: 684: 669: 663: 662: 660: 658: 652: 641: 633: 627: 626: 620: 612: 610: 609: 603: 597:. 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The 232: 224: 222: 220: 216: 215:Schempp-Hirth 212: 209: 205: 195: 191: 186: 183: 182:Schempp-Hirth 180: 178: 174: 170: 166: 162: 159: 155: 150: 146:Discus-2a 15m 143: 138: 133: 124: 121: 113: 110:December 2012 102: 99: 95: 92: 88: 85: 81: 78: 74: 71: â€“  70: 66: 65:Find sources: 59: 55: 49: 48: 43:This article 41: 37: 32: 31: 19: 1515:Not assigned 1499: 1028:Cargo glider 844: 707:. Retrieved 703: 693: 681:. Retrieved 677:the original 667: 655:. Retrieved 648:the original 643: 631: 606:. Retrieved 599:the original 586: 561:. 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Schempp-Hirth TG-15B Discus 2

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Standard-class
Manufacturer
Schempp-Hirth
Standard Class
sailplane
Schempp-Hirth
Schempp-Hirth Discus
wing section
dihedral
Winglets
Rolladen-Schneider LS8
Alexander Schleicher ASW 28
2-stroke
2-stroke
front electric sustainer
Aspect ratio
Airfoil

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