Knowledge (XXG)

SZD-12 Mucha 100

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Flight trials commenced on 14 November 1953 in Krosno (first flight by Adam Zientek); a tendency to control surface flutter was resolved by mass balancing. After this and other improvements, the Mucha 100 was cleared for production as the SZD-12 Mucha 100. From 1954, 256 were built in ZSLS in Krosno,
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Constructed from wood/plywood throughout, the Mucha 100 was much improved from the IS-2 Mucha, with smoother surfaces, better aerodynamics and comprehensive instruments and equipment including a KF-18 oxygen system, lighting and instruments for cloud flying. Pilot comfort was improved by slightly
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Further improvements were incorporated into the SZD-12A Mucha 100A, which had the external mass balances replaced by weights in the leading edges of the ailerons, forward of the hinges. Another modification which was also applied retrospectively to earlier units was a re-located mainwheel, moved
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style airbrakes of the IS-2, external mass balances fitted to the ailerons cured the tendency to flutter. The wing incidence was reduced to 2° to better align the fuselage with the airflow at higher speeds, reducing drag. Main designer was
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70 Mucha 100's were exported, mostly to the USSR, DDR, Italy, Switzerland and China in multiple orders; single examples were also exported to Austria, France, Finland and India.
545:(in English, French, and German) (1st ed.). Zurich: Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue. pp. 124–128. 514:(in English, French, and German) (1st ed.). Zurich: Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue. pp. 124–128. 202: 593: 1022: 661: 608: 153: 91: 939: 185:
throughout Poland. Two hundred and ninety were built with 73 exported to several countries and an unknown number were licence-built in the
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reclining the seat back and increasing legroom, and visibility was increased through a larger one-piece cockpit canopy.
431: 881: 871: 320: 991: 263:– modified version with altered undercarriage arrangement and internal aileron mass balances, 186 built from 1958 530:
Simons, Martin. Sailplanes 1945-1965 2nd revised edition. EQIP Werbung und Verlag G.m.b.H.. Königswinter. 2006.
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Simons, Martin. Sailplanes 1945-1965 2nd revised edition. EQIP Werbung und Verlag G.m.b.H.. Königswinter. 2006.
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http://www.aviationmuseum.eu/World/Europe/Poland/Krakow/Muzeum_Lotnictwa_Polskiego.htm
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The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs dans Le Monde
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The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs dans Le Monde
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rearwards to reduce the weight on the tailwheel during ground handling.
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World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde
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As for 1970s at least - Babiejczuk and Grzegorzewski, op.cit.
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http://www.muzeumlotnictwa.pl/zbiory_sz.php?ido=89&w=a
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0.76 m/s (150 ft/min) at 62 km/h (39 mph, 33 kn)
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Shenstone, B.S.; K.G. Wilkinson; Peter Brooks (1958).
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Shenstone, B.S.; K.G. Wilkinson; Peter Brooks (1958).
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Aircraft of comparable role, configuration, and era
157:- Glider Experimental Works) was a single-seat 587: 487:Babiejczuk, Janusz and Grzegorzewski, Jerzy. 8: 381:24 at 70 km/h (43 mph; 38 kn) 459: 457: 455: 453: 451: 449: 276:http://www.piotrp.de/SZYBOWCE/pszd12.htmThe 594: 580: 572: 363:220 km/h (137 mph, 119 kn) 218:. The prototype was made in ZSLS No.5 in 665:/ PZL Bielsko-Biała / Allstar PZL Glider 557:http://www.piotrp.de/SZYBOWCE/pszd12.htm 426: 424: 422: 420: 491:. Warsaw: Wydawnictwo MON, 1974, p. 122 416: 257:– initial production version, 104 built 369:55 km/h (34 mph, 30 kn) 18: 527:. Studio Editions: London. p. 29 480: 478: 476: 7: 489:Polski przemysł lotniczy 1945-1973 72:glider production works (ZSLS) in 14: 298:7.0 m (23 ft 0 in) 268:Specifications (SZD-12 Mucha 100) 310:1.6 m (5 ft 3 in) 304:15 m (49 ft 3 in) 27: 662:Szybowcowy Zakład Doświadczalny 525:Jane's Encyclopedia of Aviation 316:15 m (161 sq ft) 161:that was designed and built in 154:Szybowcowy Zakład Doświadczalny 16:Polish single-seat glider, 1953 1: 1023:Aircraft first flown in 1953 177:) 100 was derived from the 1039: 523:Taylor, J. H. (ed) (1989) 187:People's Republic of China 992:PZL Krosno KR-03 Puchatek 960:Margański & Mysłowski 348:290 kg (639 lb) 342:195 kg (430 lb) 119:290 + Chinese production 35: 26: 21: 602:Polish post-1945 gliders 36:SZD-12 Mucha 100 at the 1013:1950s Polish sailplanes 922:Politechnika Warszawska 432:"SZD-12 Mucha 100 (PL)" 283:General characteristics 38:Polish Aviation Museum 609:Instytut Szybownictwa 140:SZD-22 Mucha Standard 379:Maximum glide ratio: 210:, constructors were 403:Slingsby Skylark 2 261:SZD-12A Mucha 100A 173:The SZD-12 Mucha ( 109:Polish aero clubs 106:Primary user 1000: 999: 208:Władysław Okarmus 145: 144: 101:14 November 1953 22:SZD-12 Mucha 100 1030: 596: 589: 582: 573: 546: 516: 515: 507: 501: 498: 492: 486: 482: 471: 461: 444: 443: 438:. Archived from 428: 356: 285: 255:SZD-12 Mucha 100 149:SZD-12 Mucha 100 126: 116: 59: 51:Type of aircraft 31: 19: 1038: 1037: 1033: 1032: 1031: 1029: 1028: 1027: 1003: 1002: 1001: 996: 977: 954: 916: 664: 656: 603: 600: 553: 540: 520: 519: 509: 508: 504: 499: 495: 484: 483: 474: 462: 447: 430: 429: 418: 413: 394: 352: 281: 270: 251: 216:Zbigniew Badura 171: 159:glider aircraft 124: 114: 58:National origin 57: 52: 48:Glider aircraft 17: 12: 11: 5: 1036: 1034: 1026: 1025: 1020: 1015: 1005: 1004: 998: 997: 995: 994: 988: 986: 979: 978: 976: 975: 970: 964: 962: 956: 955: 953: 952: 947: 942: 937: 932: 926: 924: 918: 917: 915: 914: 909: 904: 899: 894: 889: 884: 879: 874: 869: 864: 859: 854: 849: 844: 839: 834: 829: 824: 819: 814: 809: 804: 799: 794: 789: 784: 779: 774: 769: 764: 759: 754: 749: 744: 739: 734: 729: 724: 719: 714: 709: 704: 699: 694: 689: 684: 679: 674: 668: 666: 658: 657: 655: 654: 649: 644: 639: 634: 629: 624: 619: 613: 611: 605: 604: 601: 599: 598: 591: 584: 576: 570: 569: 564: 559: 552: 551:External links 549: 548: 547: 538: 528: 518: 517: 502: 493: 472: 445: 442:on 2003-05-07. 415: 414: 412: 409: 406: 405: 393: 390: 389: 388: 382: 376: 370: 364: 361:Maximum speed: 350: 349: 343: 337: 326: 317: 311: 305: 299: 293: 269: 266: 265: 264: 258: 250: 247: 179:IS-2 Mucha-ter 170: 167: 143: 142: 137: 133: 132: 127: 125:Developed from 121: 120: 117: 111: 110: 107: 103: 102: 99: 95: 94: 89: 85: 84: 70: 66: 65: 60: 54: 53: 50: 45: 41: 40: 33: 32: 24: 23: 15: 13: 10: 9: 6: 4: 3: 2: 1035: 1024: 1021: 1019: 1016: 1014: 1011: 1010: 1008: 993: 990: 989: 987: 984: 980: 974: 971: 969: 966: 965: 963: 961: 957: 951: 948: 946: 943: 941: 938: 936: 933: 931: 928: 927: 925: 923: 919: 913: 910: 908: 905: 903: 900: 898: 895: 893: 890: 888: 885: 883: 880: 878: 875: 873: 870: 868: 865: 863: 860: 858: 855: 853: 850: 848: 845: 843: 840: 838: 835: 833: 830: 828: 825: 823: 820: 818: 815: 813: 810: 808: 805: 803: 800: 798: 795: 793: 790: 788: 785: 783: 780: 778: 775: 773: 770: 768: 765: 763: 760: 758: 755: 753: 750: 748: 745: 743: 740: 738: 735: 733: 730: 728: 725: 723: 720: 718: 715: 713: 710: 708: 705: 703: 700: 698: 695: 693: 690: 688: 685: 683: 680: 678: 675: 673: 670: 669: 667: 663: 659: 653: 650: 648: 645: 643: 640: 638: 635: 633: 630: 628: 625: 623: 620: 618: 615: 614: 612: 610: 606: 597: 592: 590: 585: 583: 578: 577: 574: 568: 565: 563: 560: 558: 555: 554: 550: 544: 539: 537: 536:3-9807977-4-0 533: 529: 526: 522: 521: 513: 506: 503: 497: 494: 490: 481: 479: 477: 473: 470: 469:3-9807977-4-0 466: 460: 458: 456: 454: 452: 450: 446: 441: 437: 436:www.piotrp.de 433: 427: 425: 423: 421: 417: 410: 408: 404: 401: 400: 399: 398: 391: 386: 385:Rate of sink: 383: 380: 377: 374: 371: 368: 365: 362: 359: 358: 357: 355: 347: 346:Gross weight: 344: 341: 340:Empty weight: 338: 336: 333: 331: 327: 324: 322: 318: 315: 312: 309: 306: 303: 300: 297: 294: 291: 288: 287: 286: 284: 279: 277: 274: 267: 262: 259: 256: 253: 252: 248: 246: 243: 239: 237: 233: 227: 225: 221: 217: 213: 209: 204: 201:replaced the 200: 196: 195:Schempp-Hirth 190: 188: 184: 180: 176: 168: 166: 164: 160: 156: 155: 150: 141: 138: 135: 134: 131: 128: 123: 122: 118: 113: 112: 108: 105: 104: 100: 98:First flight 97: 96: 93: 90: 88:Design group 87: 86: 83: 79: 75: 71: 69:Manufacturer 68: 67: 64: 61: 56: 55: 49: 46: 43: 42: 39: 34: 30: 25: 20: 1018:SZD aircraft 706: 542: 524: 511: 505: 496: 488: 440:the original 435: 407: 396: 395: 384: 378: 372: 367:Stall speed: 366: 360: 353: 351: 345: 339: 328: 321:Aspect ratio 319: 313: 307: 301: 295: 289: 282: 280: 272: 271: 260: 254: 244: 240: 228: 191: 174: 172: 152: 148: 146: 115:Number built 485:(in Polish) 354:Performance 335:NACA 43012A 181:for use by 169:Development 165:from 1953. 1007:Categories 411:References 314:Wing area: 234:and 20 in 183:aero clubs 130:IS-2 Mucha 973:Swift S-1 968:MDM-1 Fox 373:g limits: 302:Wingspan: 273:Data from 212:Jan Dyrek 199:airbrakes 136:Variants 392:See also 249:Variants 330:Airfoil 308:Height: 296:Length: 236:Wrocław 224:Bielsko 189:(PRC). 82:Wrocław 985:Krosno 912:SZD-59 907:SZD-56 902:SZD-55 897:SZD-54 892:SZD-52 887:SZD-51 882:SZD-50 877:SZD-49 872:SZD-48 867:SZD-45 862:SZD-43 857:SZD-42 852:SZD-41 847:SZD-40 842:SZD-39 837:SZD-38 832:SZD-37 827:SZD-36 822:SZD-35 817:SZD-34 812:SZD-33 807:SZD-32 802:SZD-31 797:SZD-30 792:SZD-29 787:SZD-28 782:SZD-27 777:SZD-26 772:SZD-25 767:SZD-24 762:SZD-23 757:SZD-22 752:SZD-21 747:SZD-20 742:SZD-19 737:SZD-18 732:SZD-17 727:SZD-16 722:SZD-15 717:SZD-14 712:SZD-13 707:SZD-12 702:SZD-11 697:SZD-10 534:  467:  232:Gdańsk 230:14 in 220:Krosno 197:style 163:Poland 78:Gdańsk 74:Krosno 63:Poland 692:SZD-9 687:SZD-8 682:SZD-7 677:SZD-6 672:SZD-C 290:Crew: 44:Role 950:PW-6 945:PW-5 940:PW-4 935:PW-3 930:PW-2 652:IS-C 647:IS-B 642:IS-A 637:IS-5 632:IS-4 627:IS-3 622:IS-2 617:IS-1 532:ISBN 465:ISBN 214:and 147:The 80:and 983:PZL 203:DFS 175:Fly 92:SZD 1009:: 475:^ 448:^ 434:. 419:^ 325:15 238:. 226:. 76:, 595:e 588:t 581:v 332:: 323:: 292:1 151:(

Index


Polish Aviation Museum
Glider aircraft
Poland
Krosno
Gdańsk
Wrocław
SZD
IS-2 Mucha
SZD-22 Mucha Standard
Szybowcowy Zakład Doświadczalny
glider aircraft
Poland
IS-2 Mucha-ter
aero clubs
People's Republic of China
Schempp-Hirth
airbrakes
DFS
Władysław Okarmus
Jan Dyrek
Zbigniew Badura
Krosno
Bielsko
Gdańsk
Wrocław
http://www.piotrp.de/SZYBOWCE/pszd12.htmThe
Aspect ratio
Airfoil
NACA 43012A

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