Knowledge (XXG)

Schweizer SGS 1-23

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The HM was built by using a stock 1-23H fuselage and tail assembly. Starr built a new set of 54 foot (16.6 m) span wings with an aspect ratio of 23.5:1. The wings took 1500 hours to construct, but the resulting aircraft has a glide ratio of 33.2:1 which is a 7% improvement over the stock 1-23H. The
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The "C" was subsequently sold to by Larry Gehrlein who modified it to a large degree. It was crashed and rebuilt with a set of 1-23D wings. It was later damaged again in an accident and rebuilt by the factory as a "D" model. In the mid-1980s it was owned by the Rochester Soaring
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The "C" model was also built in 1952 and, like the "B", incorporated a longer wing with a 50 foot span. The "C" had heavier wing skins and a heavier spar and, as a result, weighed 90 lbs more than the "B". There was only one "C" model built for the designer
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The 1-23G was the production version of the 1-23E and F. It retained the 52.8 foot wing and had the same glide ratio of 31:1 at 46 mph and a minimum sink speed of 1.95 feet per second at 40 mph. The "G" had a redesigned taller fin and top-surface spoilers
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The original "standard" 1-23 was introduced in 1948. The aircraft quickly became the most numerous competition and performance sailplane in the USA. A total of 93 of all sub-models were built by the time production was completed in 1967.
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The "B" model was introduced in 1952 and incorporated a longer wing of 50 feet in span. The spars were standard 1-23 spars with a spliced section added. There was only one "B" model built. It was a custom order for
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Gross weight for serial numbers 1 to 11 was 600 lbs. Later 1-23 standards had a gross weight of 660 lbs. One "standard" was retrofitted at the factory with water ballast for Kim Scribner. There were 22 "standards"
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The 1-23H was designed by adding balanced dive brakes to the "G", designing a square fin and rudder to replace the rounded ones found on earlier models, adding removable wingtips plus other minor changes.
379:, United Kingdom. He flew the "E" to a fourth place finish. The aircraft was originally constructed without a wheel and used a skid for takeoff and landing. After the Worlds a wheel was retrofitted. 349:
The "D" has a wingspan of 50 feet and a glide ratio of 30:1 at 48 mph, with a minimum sink of 2.0 feet per second at 36 mph. The gross weight on the "D" and later models is 750 lbs.
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The type received its type certificate on 13 March 1961 and a total of 47 were built, including 39 H-15s. Production of the "H" ended in 1967, completing a 19-year production run.
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Schweizer Aircraft started construction of the 1-23 prototype in May 1948. The aircraft was completed and first flew on 5 July 1948, only nine weeks after construction had begun.
1188:(in English, French, and German) (1st ed.). Zurich: Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue. pp. 234–237. 200:
Paul Bikle flew the sole 1-23E to a world absolute altitude record of 46,267 feet for a record gain of 42,300 feet on 25 February 1961. The records were set in the
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The first production 1-23 was ordered by E.J Reeves. The success of this aircraft led to more orders and series production was commenced. The 1-23 was initially sold on a "
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The original 1-23 model is also referred to as a "standard". The aircraft had a 43.83 foot wingspan and a glide ratio of 27:1, with a minimum sink of 2.3 feet per second.
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1-23Ds were flown by Paul McCready to win the 1953 US Nationals and to set a distance record of 455.5 miles (733 km) by Joe Lincoln. Lincoln was awarded the
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The 1-23E has 52.8 foot wings equipped with balanced dive brakes. It has a glide ratio of 31:1 at 46 mph and a minimum sink speed of 1.95 feet per second at 40 mph.
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and he used it to set two world altitude records on 25 February 1961. In the mid-1980s it was owned by the Rochester Soaring Club. The 1-23E was not certified.
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The 1-23D was introduced in 1953 and incorporated the improvements tested in the "B" and "C" models at the 1952 World Championships and beyond.
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A 1-23, flown by William Ivans, set a world altitude record for gliders on 30 December 1950, reaching a height of 42,089 ft (12,840 m).
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The 1-23F was a 1-23E with the same 52.8 foot wings but was constructed with heavier gauge, butt-constructed wing skins. Only one was built.
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The "H-15" reduced the span from 52.8 feet to 49.2 feet (15.0 m) which, combined with the dive-brakes, qualified the type for the then new
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Many pilots like the faster roll and better circling characteristics of the "standard" over the later longer-winged versions of the 1-23.
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In its Standard Class configuration the "H-15" has a 29:1 glide ratio at 50 mph and a minimum sink of 2.2 feet per second at 37 mph.
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The aircraft is registered as N94298 and is currently owned by Vincent Grisemer. It is on loan to the
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A total of 12 "D" models were produced. The aircraft received its type certificate on 1 June 1953.
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A total of eight 1-23Gs were constructed. The type received its type certificate on 12 June 1958.
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and the aircraft was available for him to fly it in the second half of the US Nationals.
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The production version of the "B" model was the "D" model. The 1-23B was not certified.
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with full air-brakes at max all-up weight 140 mph; 121 kn (225 km/h)
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The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume II
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The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume II
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123.0 ft/min (0.625 m/s) at 37.3 mph; 32.4 kn (60 km/h)
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in the "racing-exhibition" category by Sterling Starr and designated SGS 1-23HM.
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In April 2008 there were still 49 1-23s registered in the USA and 5 in Canada.
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to produce an aircraft with a 53.5 foot wing span and a glide ratio of 32:1.
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Said, Bob (November 1983). "1983 Sailplane Directory, Soaring Magazine".
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Said, Bob (November 1983). "1983 Sailplane Directory, Soaring Magazine".
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The type certificate is currently held by K & L Soaring of
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Wings Like Eagles, The Story of Soaring in the United States
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Wings Like Eagles, The Story of Soaring in the United States
727:. Washington, D.C.: Smithsonian Institution Press. p.  913: 401:
The 1-23F received its type certificate on 12 June 1958.
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Said, Bob (November 1983). "1983 Sailplane Directory".
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The "C" wings were also later rebuilt and used in the
1101:. Hobbs, New Mexico: Soaring Society of America: 64. 1033:. Hobbs, New Mexico: Soaring Society of America: 43. 652:
30.8:1 at 50.3 mph; 43.7 kn (81 km/h)
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Aircraft of comparable role, configuration, and era
720: 154:The prototype had been ordered by Bill Frutchy of 959:, page 183. Smithsonian Institution Press, 1988. 319:. The Precursor mounts the 1-23C wings high on a 834: 832: 830: 828: 826: 824: 822: 820: 818: 816: 814: 812: 810: 794: 792: 790: 788: 786: 784: 782: 780: 778: 776: 774: 772: 770: 768: 1120:"FAA Registry N-Number Inquiry Results N94298" 766: 764: 762: 760: 758: 756: 754: 752: 750: 748: 465:The 1-23HM was flown in the 1966 US nationals. 1222: 487:– 1-23D, N91899, and the sole 1-23HM, N94298. 8: 460:HM later had retractable landing gear added. 714: 712: 710: 708: 706: 634:67.7 mph; 58.9 kn (109 km/h) 1229: 1215: 1207: 615:140 mph (225 km/h, 121 kn) 1202:Detailed photos of a SGS 1-23D in the NSM 1110: 1108: 622:140 mph; 121 kn (225 km/h) 367:A single 1-23E model was constructed for 1184:Shenstone, B.S.; K.G. Wilkinson (1963). 628:110 mph; 96 kn (177 km/h) 702: 664:4.5 lb/sq ft (22.2 kg/m) 450:One production 1-23H was rebuilt as an 1162: 1139: 1137: 1135: 925: 883: 881: 646:+6 -4 at 125.3 kn (232 km/h) 545:164.94 sq ft (15.323 m) 533:52 ft 8.0 in (16.052 m) 384:The aircraft was subsequently sold to 26: 879: 877: 875: 873: 871: 869: 867: 865: 863: 861: 527:20 ft 5.4 in (6.232 m) 123:is a United States Open and Standard 7: 803:. Soaring Society of America: 28–30. 539:3 ft 6.7 in (1.085 m) 1005:"Canadian Civil Aircraft Register" 197:in 1960 for that distance flight. 25: 288:specifically to fly in the 1952 262:specifically to fly in the 1952 170:Civil Aeronautics Administration 35: 1116:Federal Aviation Administration 1069:Federal Aviation Administration 1045:Federal Aviation Administration 977:Federal Aviation Administration 889:Federal Aviation Administration 1579:1940s United States sailplanes 1146:"Sailplanes in Our Collection" 893:"GLIDER SPECIFICATION NO. 1G1" 84:Schweizer Aircraft Corporation 1: 1594:Aircraft first flown in 1948 301:The 1-23C was not certified. 373:World Gliding Championships 290:World Gliding Championships 264:World Gliding Championships 249:There were no 1-23As built. 1615: 912:K & L Soaring (n.d.). 719:Schweizer, Paul A (1988). 597:750 lb (340 kg) 591:481 lb (218 kg) 175:1G1 on 22 November 1949. 43: 34: 29: 1558:William (Bill) Schweizer 1245:Sailplanes & Gliders 914:"K & L Soaring, LLC" 127:, single-seat, mid-wing 1499:Reconnaissance Aircraft 839:Activate Media (2006). 512:General characteristics 500:Specifications (1-23-H) 485:National Soaring Museum 472:National Soaring Museum 371:to compete in the 1954 340: 147:Design and development 1431:Agricultural Aircraft 1073:"FAA Registry N94298" 946:Bridgman 1951, p. 6b. 452:experimental aircraft 338: 1169:: CS1 maint: year ( 932:: CS1 maint: year ( 841:"SGS 1-23 Schweizer" 650:Maximum glide ratio: 620:Rough air speed max: 213:Inyokern, California 44:Schweizer SGS 1-23D 1452:Amphibious Aircraft 1144:Munson, J. (n.d.). 955:Schweizer, Paul A: 632:Winch launch speed: 493:El Mirador airfield 479:Aircraft on display 186:Operational history 1584:Schweizer aircraft 1238:Schweizer Aircraft 891:(September 2007). 638:Terminal velocity: 611:Never exceed speed 420:1-23H and 1-23H-15 341: 317:Gehrlein Precursor 209:Mojave, California 168:The 1-23 received 133:Schweizer Aircraft 121:Schweizer SGS 1-23 1589:Mid-wing aircraft 1566: 1565: 1516:RU-38 Twin Condor 117: 116: 16:(Redirected from 1606: 1553:Paul A Schweizer 1548:Ernest Schweizer 1231: 1224: 1217: 1208: 1190: 1189: 1181: 1175: 1174: 1168: 1160: 1158: 1157: 1148:. Archived from 1141: 1130: 1129: 1127: 1126: 1112: 1103: 1102: 1099:Soaring Magazine 1094: 1083: 1082: 1080: 1079: 1065: 1059: 1058: 1056: 1055: 1041: 1035: 1034: 1031:Soaring Magazine 1026: 1020: 1019: 1017: 1016: 1007:. 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Archived from 836: 805: 804: 801:Soaring Magazine 796: 743: 742: 726: 716: 605: 514: 495:- 1-23h, ZS-GDN. 286:Paul A Schweizer 195:Barringer Trophy 180:Cayuta, New York 173:type certificate 156:Elmira, New York 137:Elmira, New York 110: 94:Paul A Schweizer 72: 64:Type of aircraft 39: 27: 21: 1614: 1613: 1609: 1608: 1607: 1605: 1604: 1603: 1599:Glider aircraft 1569: 1568: 1567: 1562: 1536: 1532:MQ-8 Fire Scout 1520: 1494: 1463: 1447: 1426: 1240: 1235: 1198: 1193: 1183: 1182: 1178: 1161: 1155: 1153: 1143: 1142: 1133: 1124: 1122: 1114: 1113: 1106: 1096: 1095: 1086: 1077: 1075: 1067: 1066: 1062: 1053: 1051: 1043: 1042: 1038: 1028: 1027: 1023: 1014: 1012: 999: 998: 994: 985: 983: 975: 974: 970: 954: 950: 945: 941: 924: 918: 916: 911: 910: 906: 897: 895: 887: 886: 859: 850: 848: 838: 837: 808: 798: 797: 746: 739: 718: 717: 704: 700: 692:List of gliders 671: 616: 601: 510: 502: 481: 339:Schweizer 1-23D 321:Schweizer 1-26A 224: 188: 149: 113:93 (all marks) 108: 71:National origin 70: 65: 23: 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Index

Schweizer 1-23

Open-class
Standard-class
sailplane
Schweizer Aircraft Corporation
Paul A Schweizer
Class
glider
Schweizer Aircraft
Elmira, New York
Elmira, New York
factory direct
Civil Aeronautics Administration
type certificate
Cayuta, New York
Barringer Trophy
Sierra Nevada
lee wave
Mojave, California
Inyokern, California
Paul MacCready
World Gliding Championships
Madrid
Paul A Schweizer
World Gliding Championships
Madrid
homebuilt
Gehrlein Precursor
Schweizer 1-26A

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