Knowledge (XXG)

RWD 21

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26: 323: 310: 191:. In spite of the designation, the RWD 16bis design was new, only partly basing on the RWD 16 construction. On contrary, it appeared a successful design, with good handling and performance and ease of flying. It was a wooden low-wing monoplane, with two seats side-by-side in a closed cockpit. 217:
and some minor changes, mostly to a canopy. The prototype was flown in February 1939 (registration SP-BPE). The first series of 10 aircraft was ordered and at least six were completed and registered before the war outbreak (SP-BRE, BRF, BRG, BRH, BRM, KAR)
251:, who had not flown a plane before). At least one of them (SP-BPE) was used in Romania with markings YR-VEN and returned to Poland after the war. It was next used until the mid-1950s with new markings SP-AKG. It is currently restored and preserved in the 242:
Aero Club (SP-BRF), three by the LOPP (SP-BRE, BRG, BRH), one by private owner (SP-KAR) and two remained in the factory (SP-BPE, BRM). After the German invasion on Poland, in September 1939, two RWD 21s (SP-BPE and BRM) were evacuated from the factory to
235:(including the engine 6,200 zł), in order to sell airframes to private owners for 9,500 zł (the price of a mid-class car), lending them engines. The price of the RWD 21 was 20,500 zł (including the engine 8,000 zł). 230:
paramilitary organization as successful economical planes, suitable for the plan of subsidising the development of private aviation in Poland. A series of RWD 16bis was ordered by the LOPP at a price of 17,800
290:, plywood (fins) and canvas (elevators and rudder) covered. Two seats side-by-side, with twin controls, under a canopy, with a fixed windshield. Behind a cockpit, a place for a baggage. Conventional fixed 298:
in front, driving a two-blade fixed pitch Szomański wooden propeller, with a 73 L (19 US gal; 16 imp gal) fuel tank in the centre-section, under the crew seats.
206:
paramilitary organization ordered 20 aircraft, the first were to be built by May 1939. Probably a few were completed by the outbreak of the World War II, but there are no evidences.
282:, plywood-covered, duralumin in front engine section. Single-part trapezoid wings with rounded tips, two-spar, plywood (in front) and canvas covered, fitted with split 198:(registration SP-BNM) followed by the second prototype (SP-BPC). Both were powered by a Polish-designed 63 hp Avia 3 straight engine. In series, a 62 hp 874: 889: 438:
73 L (19 US gal; 16 imp gal) in a centre-section tank ; 7 L (1.8 US gal; 1.5 imp gal) oil
717: 894: 869: 65: 656: 25: 187:
bureau as a light and economical touring and sports plane, utilizing the experience from an unsuccessful earlier design
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bureau, sharing the same construction, main difference of the RWD 21 being a stronger engine.
848: 195: 180: 86: 295: 283: 278:, conventional in layout, with a fixed landing gear and a closed cockpit. Fuselage semi- 863: 798: 199: 557: 291: 163:
two-seat low-wing touring and sports planes of the late 1930s, constructed by the
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4-cylinder air-cooledinverted in-line piston engine, 67 kW (90 hp)
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was a development variant with a stronger 90 hp engine
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The first prototype was built and first flown in June–July
238:
At the outbreak of World War II, one RWD 21 was owned by
469:
210 km/h (130 mph, 110 kn) at sea level
294:
with a rear skid, the main gear in covers. 4-cylinder
499:
1,000 m (3,300 ft) in 4 minutes 30 seconds
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Aircraft of comparable role, configuration, and era
640: 585:"Produkcja samolotów i szybowców w S.L. i D.W.L." 711: 8: 676:(in Polish). Warsaw: WKiŁ. pp. 322–323. 718: 704: 696: 475:175 km/h (109 mph, 94 kn) 454:2-bladed Szomański fixed-pitch propeller 274:Wooden construction low-wing cantilever 548: 505:44.1 kg/m (9.0 lb/sq ft) 487:600 km (370 mi, 320 nmi) 674:Polskie konstrukcje lotnicze 1893–1939 481:72 km/h (45 mph, 39 kn) 353:Polskie konstrukcje lotnicze 1893–1939 15: 607: 605: 514:0.1021 kW/kg (0.0621 hp/lb) 202:II straight engine was expected. The 7: 398:14.95 m (160.9 sq ft) 875:1930s Polish civil utility aircraft 691:Photos and drawings at Ugolok Neba 410:Warsaw Aerodynamic Institute 16%; 392:2.12 m (6 ft 11 in) 14: 414:Warsaw Aerodynamic Institute 10%; 380:8.4 m (27 ft 7 in) 386:11 m (36 ft 1 in) 321: 308: 226:Both aircraft were found by the 24: 890:Single-engined tractor aircraft 266:, its further fate is unknown. 247:(one of them by a glider pilot 1: 493:5,500 m (18,000 ft) 895:Aircraft first flown in 1938 262:One RWD 21 was evacuated to 870:1930s Polish sport aircraft 432:685 kg (1,510 lb) 426:660 kg (1,455 lb) 183:by Andrzej Anczutin of the 911: 350:Polish aircraft 1893-1939, 286:. Conventional cantilever 734: 643:Polish aircraft 1893-1939 420:425 kg (937 lb) 32: 23: 18: 336:Royal Romanian Air Force 44:Touring and sports plane 672:Glass, Andrzej (1977). 359:General characteristics 342:Specifications (RWD-21) 639:Cynk, Jerzy B (1971). 446:Blackburn Cirrus Minor 253:Polish Aviation Museum 35:Polish Aviation Museum 249:Bronisław Żurakowski 647:. Putnam. pp.  620:(in Polish). Warsaw 590:(in Polish). Warsaw 430:Max takeoff weight: 222:Operational history 110:Primary user 885:Low-wing aircraft 857: 856: 614:"Skrzydla Polski" 497:Time to altitude: 149: 148: 902: 720: 713: 706: 697: 678: 677: 669: 663: 662: 646: 636: 630: 629: 627: 625: 612:Gujski, Robert. 609: 600: 599: 597: 595: 583:Gujski, Robert. 580: 574: 573: 571: 569: 556:Gujski, Robert. 553: 491:Service ceiling: 462: 361: 327: 325: 324: 314: 312: 311: 179:was designed in 140: 131:>2 RWD 16bis 128: 54: 46:Type of aircraft 28: 16: 910: 909: 905: 904: 903: 901: 900: 899: 860: 859: 858: 853: 730: 724: 687: 682: 681: 671: 670: 666: 659: 638: 637: 633: 623: 621: 611: 610: 603: 593: 591: 582: 581: 577: 567: 565: 555: 554: 550: 545: 521: 458: 357: 344: 322: 320: 309: 307: 304: 296:straight engine 272: 224: 173: 138: 132: 126: 53:National origin 52: 47: 12: 11: 5: 908: 906: 898: 897: 892: 887: 882: 877: 872: 862: 861: 855: 854: 852: 851: 846: 841: 836: 831: 826: 821: 816: 811: 806: 801: 796: 791: 786: 781: 776: 771: 766: 761: 756: 751: 746: 741: 735: 732: 731: 725: 723: 722: 715: 708: 700: 694: 693: 686: 685:External links 683: 680: 679: 664: 657: 631: 601: 575: 547: 546: 544: 541: 538: 537: 532: 520: 517: 516: 515: 506: 500: 494: 488: 482: 476: 470: 467:Maximum speed: 456: 455: 449: 439: 436:Fuel capacity: 433: 427: 421: 415: 399: 393: 387: 381: 375: 369: 343: 340: 339: 338: 332: 331: 318: 303: 300: 271: 268: 223: 220: 172: 169: 147: 146: 141: 139:Developed from 135: 134: 129: 123: 122: 119: 115: 114: 111: 107: 106: 103: 99: 98: 95: 91: 90: 84: 80: 79: 73: 69: 68: 63: 59: 58: 55: 49: 48: 45: 42: 38: 37: 33:RWD 21 in the 30: 29: 21: 20: 13: 10: 9: 6: 4: 3: 2: 907: 896: 893: 891: 888: 886: 883: 881: 878: 876: 873: 871: 868: 867: 865: 850: 847: 845: 842: 840: 837: 835: 832: 830: 827: 825: 822: 820: 817: 815: 812: 810: 807: 805: 802: 800: 799:RWD 14 Czapla 797: 795: 792: 790: 787: 785: 782: 780: 777: 775: 772: 770: 767: 765: 762: 760: 757: 755: 752: 750: 747: 745: 742: 740: 737: 736: 733: 728: 721: 716: 714: 709: 707: 702: 701: 698: 692: 689: 688: 684: 675: 668: 665: 660: 658:0-370-00085-4 654: 650: 645: 644: 635: 632: 619: 615: 608: 606: 602: 589: 586: 579: 576: 563: 559: 552: 549: 542: 540: 536: 533: 531: 530:Bücker Bü 181 528: 527: 526: 525: 518: 513: 511: 507: 504: 503:Wing loading: 501: 498: 495: 492: 489: 486: 483: 480: 477: 474: 473:Cruise speed: 471: 468: 465: 464: 463: 461: 453: 450: 447: 443: 440: 437: 434: 431: 428: 425: 424:Gross weight: 422: 419: 418:Empty weight: 416: 413: 409: 406: 404: 400: 397: 394: 391: 388: 385: 382: 379: 376: 373: 370: 367: 364: 363: 362: 360: 355: 354: 351: 348: 341: 337: 334: 333: 330: 319: 317: 306: 305: 301: 299: 297: 293: 289: 285: 281: 277: 269: 267: 265: 260: 258: 254: 250: 246: 241: 236: 234: 229: 221: 219: 216: 212: 207: 205: 201: 200:Walter Mikron 197: 192: 190: 186: 182: 178: 170: 168: 166: 162: 158: 154: 145: 142: 137: 136: 133:>6 RWD 21 130: 125: 124: 120: 117: 116: 112: 109: 108: 104: 101: 100: 96: 94:Introduction 93: 92: 88: 85: 83:First flight 82: 81: 77: 74: 71: 70: 67: 64: 62:Manufacturer 61: 60: 56: 51: 50: 43: 40: 39: 36: 31: 27: 22: 17: 880:RWD aircraft 833: 673: 667: 642: 634: 622:. Retrieved 617: 592:. Retrieved 587: 578: 566:. Retrieved 561: 558:"RWD-16 bis" 551: 539: 523: 522: 508: 502: 496: 490: 484: 479:Stall speed: 478: 472: 466: 459: 457: 451: 441: 435: 429: 423: 417: 411: 407: 401: 395: 389: 383: 377: 371: 365: 358: 356: 352: 349: 346: 345: 292:landing gear 273: 261: 237: 225: 215:Cirrus Minor 210: 208: 193: 176: 174: 156: 152: 150: 127:Number built 89:(RWD 16bis) 624:12 November 618:rwd-dwl.net 594:12 November 588:rwd-dwl.net 568:11 November 564:(in Polish) 562:rwd-dwl.net 460:Performance 452:Propellers: 442:Powerplant: 270:Description 171:Development 864:Categories 543:References 510:Power/mass 396:Wing area: 121:1938-1939 384:Wingspan: 372:Capacity: 347:Data from 302:Operators 288:empennage 280:monocoque 276:monoplane 177:RWD 16bis 153:RWD 16bis 118:Produced 72:Designer 729:aircraft 519:See also 102:Retired 649:556-561 535:LWD Żak 403:Airfoil 390:Height: 378:Length: 329:Romania 245:Romania 113:Poland 78:bureau 57:Poland 19:RWD 21 849:RWD 25 844:RWD 23 839:RWD 22 834:RWD 21 829:RWD 20 824:RWD 19 819:RWD 18 814:RWD 17 809:RWD 16 804:RWD 15 794:RWD 13 789:RWD 11 784:RWD 10 655:  485:Range: 326:  316:Poland 313:  264:Latvia 257:Kraków 211:RWD 21 189:RWD 16 161:Polish 157:RWD 21 144:RWD 16 779:RWD 9 774:RWD 8 769:RWD 7 764:RWD 6 759:RWD 5 754:RWD 4 749:RWD 3 744:RWD 2 739:RWD 1 408:root: 366:Crew: 284:flaps 240:Wilno 233:złoty 159:were 105:1950 97:1938 41:Role 653:ISBN 626:2019 596:2019 570:2019 444:1 × 412:tip: 228:LOPP 209:The 204:LOPP 196:1938 181:1938 175:The 155:and 151:The 87:1938 727:RWD 255:in 185:RWD 165:RWD 76:RWD 66:DWL 866:: 651:. 616:. 604:^ 560:. 259:. 719:e 712:t 705:v 661:. 628:. 598:. 572:. 512:: 405:: 374:1 368:1

Index


Polish Aviation Museum
DWL
RWD
1938
RWD 16
Polish
RWD
1938
RWD
RWD 16
1938
Walter Mikron
LOPP
Cirrus Minor
LOPP
złoty
Wilno
Romania
Bronisław Żurakowski
Polish Aviation Museum
Kraków
Latvia
monoplane
monocoque
flaps
empennage
landing gear
straight engine
Poland

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