281:; Gene did the majority of the construction work and the prototype was completed in about 400 hours. The prototype Quickie registered "N77Q" (77 for 1977, Q for Quickie.) started its flight test program on November 1977. All three of the designers flew it on the first day. The prototype was modified during its test program. The span of both the canard and main wing were increased to improve lifting ability. These reduced stall speed and shortened takeoff and landing distances; its attitude on the ground was also adjusted for optimal takeoff and landing. Originally designed with a fixed fin and only the faired tailwheel acting as the rudder, a conventional rudder was substituted. The steerable tailwheel allows directional control up to the point of liftoff, as the Quickie does not lift its tail during the takeoff run. Although it takes off at around 55 mph and its maximum speed of 126 mph is impressive for its engine power, the rate of climb is "modest". The flight test program was completed in mid-April 1978, five months after its first flight.
31:
220:
design and other projects, and it was Jewett and
Sheehan who continued development of the design and market it for home-build use. An agreement was reached that Rutan would fund the development and testing and once the design was complete they would pay Rutan back from future sales of the designs and
203:
intention in 1975 for a low-cost, low-power, single-seat homebuilt aircraft. The first element to be found by Jewett and
Sheehan was the engine, which – although low-powered (they had anticipated 12 hp) – had to be reliable for aviation work. With the help of Onan, a manufacturer of industrial
215:
layout. Conversely to canard layout, the conventional front engine location put the pilot close to the center of gravity, a key point for a light aircraft. The wheels were incorporated into wingtip fairings without much drag penalty and the tandem layout gave safe stalling characteristics. Rutan
309:
In June 1978, only two months after the prototype's first flight, Jewett and
Sheehan formed the Quickie Aircraft Corporation to produce and sell complete aircraft kits. Production began in June 1978, and by 1980 the Corporation had sold 350 kits. Other firms were granted marketing rights, and
268:
Pilot controls include a side-stick on the right and a throttle on the left. Rudder pedals are linked to the steerable tailwheel. The rather crude cable-operated brake comprises a cockpit lever operating steel tire-scrubbers on each main wheel.
241:
As with other Rutan designs, the
Quickie is constructed of glass fibre and resin over a foam core. The wings are foam blanks cut to shape with a hot wire before covering, and the fuselage made up of 1 inch-thick (25.4 mm) foam slabs.
211:. After a preliminary pusher canard configuration design (Rutan Model 49) had been discarded, his solution to the design issues of low drag without retractable undercarriage and a workable center of gravity travel, was a tractor engine/
257:
are located inboard on the rear wing which is shoulder-mounted just aft of the pilot. The tandem layout provides positive lift from both pairs of wings; whereas on a conventional aircraft, the tailplane mostly provides negative lift.
624:
in "Quickie-Type
Aircraft Design Origins", Rutan wrote : "While the Model 49 appeared feasible, it had potential shortcomings : very low Reynolds number on the fins and canard wing and excessive CG travel with pilot weight
216:
produced the first drawings in May 1977 and thereafter the three of them worked on the design drawings over the next two months with construction beginning in August After the first flights, Rutan spent more time with his
265:, such savings allowing a smaller engine and a smaller fuel tank. Even though the propeller is of small diameter, propeller clearance remains limited and the Quickie is rather vulnerable to ground strikes.
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taildragger, having one forward wing and one rear wing (instead of the more usual main wing and tailplane). According to Rutan this layout was not new, having previously been used in aircraft such as the
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The
Quickie has fixed (non-retractable) main wheels faired into spats located at the tips of the forward wing. The absence of separate landing gear helps to
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Corporation was formed to produce and market the
Quickie in kit form after 1978. Two years later a two-seater variant of the same layout followed as the
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four-stroke engines, they were able to procure a 70 lb (32 kg) engine that would deliver 18 hp (14 kW) at 3,600 rpm.
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The forward wing provides around 60% of the lift. The full-span control surfaces on the forward wing serve as combined
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58 mph (93 km/h, 50 kn) "pitch bucking" occurs below this speed, ailerons remain effective.
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192:(Model 54 in Rutan's design series) is one of several unconventional aircraft penned by Rutan for the
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ultimately some 1,000 Quickie kits were sold. The
Corporation closed its doors in the mid 1980s.
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236.5 lb (108 kg) useful load, pilots up to 6'5" 210lb, maximum luggage capacity 30 lb (9.1 kg)
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301:, where the aircraft drew intense public interest and won the Outstanding New Design Award.
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490–720 mi (790–1,160 km, 430–630 nmi) 121mph at 6,500' or 75mph at 10,500'
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1 × Onan B48M opposed four-stroke piston engine, 18 hp (13 kW) at 3,600 rpm
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Rutan was then involved with the design; Sheehan and Jewett suggesting a scaled-down
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rear wing. The forward wing has full-span control surfaces and is thus similar to a
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829:"Liste der auf der Museumsinsel in München ausgestellten Luftfahrzeuge"
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942:, no. 15, Rutan Aircraft Factory, January 1978, archived from
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Burt Rutan (October 1981). "Quickie-Type
Aircraft Design Origins".
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919:, no. 16, Rutan Aircraft Factory, April 1978, archived from
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47 mph (76 km/h, 41 kn) power on, 53mph power off
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Construction of the prototype commenced in August 1977 at the
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526:, two seater-variant by Quickie Aircraft Corporation
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Aircraft of comparable role, configuration, and era
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15 ft 4 in (4.67 m) canard (forward)
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16 ft 8 in (5.08 m) main wing (rear)
569:Tom Jewett (November 1981). "Point CounterPoint".
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289:In June 1978 a Quickie prototype was flown to the
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539:, two seater-variant by Viking Aircraft Company
1021:The Complete Guide to Rutan Aircraft-Chapter 6
898:
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1892:(vice president/general manager, test pilot)
1057:Rutan Aircraft Factory and Scaled Composites
577:
562:
1904:(director of flight operations, test pilot)
1950:1970s United States civil utility aircraft
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474:150 mph (240 km/h, 130 kn)
459:121 mph (195 km/h, 105 kn)
453:126 mph (203 km/h, 109 kn)
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977:, no. 17, p. 2, archived from
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995:"Quickie-type aircraft design origins"
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152:The Quickie was primarily designed by
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901:"Quickie - Lightweight Extraordinary"
677:"Canard Advantages and Disadvantages"
637:
599:
164:forward wing and one slightly larger
16:Light aircraft designed by Burt Rutan
899:Barnett, Cliff (February 14, 1979),
783:
156:as a low-powered, highly efficient
13:
817:
414:53.8 sq ft (5.00 m)
390:17 ft 4 in (5.28 m)
14:
1961:
958:
805:from the original on May 16, 2023
408:4 ft 5 in (1.35 m)
291:Experimental Aircraft Association
160:. Its tandem wing design has one
765:Canada Aviation and Space Museum
747:British Columbia Aviation Museum
325:Canada Aviation and Space Museum
320:British Columbia Aviation Museum
224:
37:Canada Aviation and Space Museum
29:
892:
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845:
757:
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634:The Canard Pusher N°15, page 11
495:425 ft/min (2.16 m/s)
351:Specifications (Prototype N77Q)
1235:Rocketcraft (as subcontractor)
695:
679:. Desktop.aero. Archived from
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145:construction, configured with
1:
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273:Construction and flight tests
137:is a lightweight single-seat
1930:Aircraft first flown in 1977
1910:(SpaceShipOne sole investor)
7:
1153:Virgin Atlantic GlobalFlyer
1131:Aircraft (as subcontractor)
993:Burt Rutan (October 1981),
499:
420:243.5 lb (110 kg)
263:reduce both weight and drag
10:
1966:
751:"The Modern Era (1970 – )"
736:Canard Pusher n°17, page 2
199:The Quickie followed from
83:, Tom Jewett, Gene Sheehan
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1406:Mojave Aerospace Ventures
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791:Canadian Museum of Flight
771:. Aviation.technomuses.ca
432:485 lb (220 kg)
426:480 lb (218 kg)
330:Canadian Museum of Flight
117:
109:
104:
96:
88:
75:
57:
49:
44:
28:
23:
1177:Technology demonstrators
556:
1319:Spirit of Steve Fossett
1065:Aircraft (main designs)
1059:aircraft and spacecraft
512:Quickie Free Enterprise
369:General characteristics
293:'s annual gathering at
285:Recognition and records
1242:McDonnell Douglas DC-X
1016:Quickie Rutan model 54
965:Original Quickie photo
855:. Airventuremuseum.org
853:"Rutan-Herron Quickie"
799:www.canadianflight.org
712:, aeroresourcesinc.com
345:New England Air Museum
295:EAA AirVenture Oshkosh
279:Rutan Aircraft Factory
176:Design and development
135:Rutan Model 54 Quickie
64:Rutan Aircraft Factory
1898:(manager, test pilot)
1401:The Spaceship Company
971:"Flight test reports"
875:"Aircraft Collection"
479:Minimum control speed
340:EAA AirVenture Museum
1945:Tandem-wing aircraft
905:Flight International
795:"Canadian Quickie 1"
651:Flight International
613:Flight International
359:Flight International
236:Mignet "Flying Flea"
201:Jewett and Sheehan's
92:kit production ended
53:Single seat aircraft
1256:Spaceflight program
1011:on December 4, 2010
767:(August 30, 2016).
545:, single-seat racer
518:Related development
430:Max takeoff weight:
314:Aircraft on display
45:General information
1935:Homebuilt aircraft
1880:(former president)
708:2015-06-10 at the
543:Rutan Amsoil racer
470:Never exceed speed
299:Oshkosh, Wisconsin
1917:
1916:
1414:
1413:
1158:Williams V-Jet II
975:The Canard Pusher
940:The Canard Pusher
917:The Canard Pusher
725:The Canard Pusher
362:The Canard Pusher
229:The Quickie is a
131:
130:
1957:
1337:Stratolaunch Roc
1304:White Knight Two
1275:White Knight One
1263:Programs / Ships
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1004:, archived from
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981:on July 31, 2013
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946:on July 31, 2013
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827:(January 2013).
825:Deutsches Museum
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683:on July 22, 2012
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537:Viking Dragonfly
506:Quickie Aircraft
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335:Deutsches Museum
194:general aviation
188:. The original
182:Quickie Aircraft
126:Viking Dragonfly
69:Quickie Aircraft
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524:QAC Quickie Q2
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122:QAC Quickie Q2
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1306:
1305:
1302:
1298:
1297:
1292:
1289:
1288:
1283:
1282:
1281:
1278:
1276:
1273:
1271:
1268:
1267:
1265:
1261:
1258:
1254:
1248:
1247:Rotary Rocket
1245:
1243:
1240:
1239:
1237:
1233:
1227:
1224:
1221:
1218:
1215:
1212:
1210:
1207:
1205:
1202:
1200:
1197:
1195:
1192:
1190:
1187:
1185:
1182:
1181:
1179:
1175:
1169:
1168:X-47A Pegasus
1166:
1164:
1161:
1159:
1156:
1154:
1151:
1149:
1146:
1144:
1141:
1139:
1136:
1135:
1133:
1129:
1123:
1120:
1118:
1115:
1113:
1110:
1108:
1105:
1103:
1100:
1098:
1095:
1093:
1090:
1088:
1085:
1083:
1080:
1078:
1075:
1073:
1070:
1069:
1067:
1063:
1058:
1051:
1046:
1044:
1039:
1037:
1032:
1031:
1028:
1022:
1019:
1017:
1014:
1007:
1003:
996:
991:
980:
976:
972:
968:
966:
963:
962:
945:
941:
937:
933:
922:
918:
914:
910:
906:
902:
897:
896:
876:
870:
854:
848:
830:
826:
820:
804:
800:
796:
792:
786:
770:
766:
760:
752:
748:
742:
733:
726:
721:
719:
711:
707:
704:
698:
682:
678:
672:
665:
659:
652:
647:
645:
643:
641:
631:
621:
614:
609:
607:
605:
603:
594:
587:
585:
583:
581:
572:
565:
561:
549:
544:
541:
538:
535:
534:
533:
532:
525:
522:
521:
520:
519:
513:
510:
507:
504:
503:
494:
491:
488:
485:
482:
480:
476:
473:
471:
467:
464:
461:
458:
457:Cruise speed:
455:
452:
449:
448:
447:
445:
437:
434:
431:
428:
425:
424:Gross weight:
422:
419:
418:Empty weight:
416:
413:
410:
407:
404:
401:
398:
395:
392:
389:
386:
383:
380:
377:
374:
373:
372:
370:
365:
363:
360:
357:
346:
343:
341:
338:
336:
333:
331:
328:
326:
323:
321:
318:
317:
311:
302:
300:
296:
292:
282:
280:
270:
266:
264:
259:
256:
252:
248:
243:
239:
237:
232:
225:Configuration
222:
219:
214:
210:
205:
202:
197:
195:
191:
187:
183:
173:
171:
167:
163:
159:
155:
150:
148:
144:
140:
136:
127:
123:
120:
116:
113:November 1977
112:
108:
103:
99:
95:
91:
87:
82:
78:
74:
70:
65:
62:
60:
56:
52:
48:
43:
38:
32:
27:
22:
19:
1896:Brian Binnie
1890:Mike Melvill
1886:(test pilot)
1470:
1318:
1310:
1295:
1286:
1280:SpaceShipTwo
1270:SpaceShipOne
1148:Toyota TAA-1
1081:
1006:the original
1001:
983:, retrieved
979:the original
974:
948:, retrieved
944:the original
939:
925:, retrieved
921:the original
916:
904:
893:Bibliography
879:. Retrieved
869:
859:November 17,
857:. Retrieved
847:
835:. Retrieved
819:
807:. Retrieved
798:
785:
773:. Retrieved
759:
741:
732:
724:
697:
685:. Retrieved
681:the original
671:
663:
658:
650:
630:
620:
612:
592:
570:
564:
548:
530:
529:
517:
516:
492:
486:
477:
468:
463:Stall speed:
462:
456:
450:
443:
441:
435:
429:
423:
417:
411:
405:
399:
393:
387:
381:
375:
368:
366:
361:
358:
355:
354:
308:
288:
276:
267:
260:
244:
240:
228:
206:
198:
189:
179:
151:
147:tandem wings
141:aircraft of
134:
132:
110:First flight
97:Number built
71:(production)
59:Manufacturer
18:
907:: 1160–1162
775:October 16,
625:variation."
508:Corporation
444:Performance
436:Powerplant:
231:tandem wing
213:tandem wing
170:canard wing
139:taildragger
66:(prototype)
1924:Categories
1908:Paul Allen
1878:Doug Shane
1872:Burt Rutan
1287:Enterprise
1222:(uncrewed)
1216:(uncrewed)
1102:Pond Racer
1072:VariViggen
552:References
412:Wing area:
305:Production
154:Burt Rutan
81:Burt Rutan
24:Quickie Q1
1874:(founder)
1220:Model 396
1214:Model 395
1138:Adam A500
1122:Model 401
1107:Boomerang
913:"Quickie"
881:March 29,
769:"Quickie"
382:Capacity:
378:One pilot
356:Data from
247:elevators
158:kit-plane
143:composite
1356:Tier One
803:Archived
793:(2023).
706:Archived
687:June 13,
500:See also
255:Ailerons
209:Vari-Eze
196:market.
166:dihedral
162:anhedral
118:Variants
76:Designer
1349:flights
1226:Vantage
1209:Triumph
1204:Grizzly
1199:Catbird
1112:Proteus
1097:Voyager
1092:Long-EZ
1087:Defiant
1082:Quickie
1077:VariEze
985:May 15,
950:May 15,
927:May 15,
809:May 16,
703:Quickie
406:Height:
388:Length:
218:Defiant
190:Quickie
105:History
877:. NEAM
837:May 7,
662:Rutan
487:Range:
364:No. 16
221:kits.
89:Status
1296:Unity
1194:BiPod
1009:(PDF)
998:(PDF)
832:(PDF)
653:p1162
615:p1161
557:Notes
376:Crew:
251:flaps
1317:VMS
1309:VMS
1294:VSS
1285:VSS
1189:ATTT
1184:ARES
1163:X-38
987:2013
952:2013
929:2013
883:2013
861:2013
839:2014
811:2023
777:2016
727:N°16
689:2012
249:and
180:The
133:The
100:350+
50:Type
1856:406
1851:401
1846:400
1841:396
1836:395
1831:375
1826:372
1821:367
1816:355
1811:351
1806:348
1801:346
1796:344
1791:343
1786:342
1781:341
1776:340
1771:339
1766:333
1761:326
1756:318
1751:316
1746:313
1741:311
1736:309
1731:302
1726:301
1721:300
1716:287
1711:281
1706:276
1701:271
1696:260
1691:257
1686:254
1681:247
1676:241
1671:233
1666:231
1661:226
1656:206
1651:205
1646:202
1641:191
1636:181
1631:179
1626:175
1621:173
1616:170
1611:169
1606:165
1601:164
1596:163
1591:158
1586:151
1581:144
1576:143
1571:133
1566:126
1561:120
1556:115
1386:17P
1381:16P
1376:15P
1371:14P
1366:13P
1361:11P
1311:Eve
666:p63
297:at
1926::
1551:97
1546:91
1541:89
1536:81
1531:79
1526:78
1521:77
1516:76
1511:74
1506:73
1501:72
1496:70
1491:68
1486:61
1481:59
1476:58
1471:54
1466:49
1461:40
1456:35
1451:33
1446:32
1441:31
1436:28
1431:27
1000:,
973:,
938:,
915:,
903:,
801:.
797:.
749:.
717:^
639:^
601:^
579:^
253:.
238:.
186:Q2
149:.
1426:1
1290:†
1049:e
1042:t
1035:v
885:.
863:.
841:.
813:.
779:.
753:.
691:.
595:.
573:.
481::
472::
39:.
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
