37:
320:
282:
to the MS.121, with its mainwheels on half-axles mounted centrally on a fixed transverse V-strut from the lower fuselage and their outer ends supported by dural-faired legs with multiple rubber ring shock absorbers from the lower longerons. The track was 1.96 m (77 in). Both variants had
128:
explored the possibilities of light fighters, with lower power and light armament but with rapid climb and long endurance. They were also less costly to build. The Jockey programme, as it became known, began in France in 1926 and Morane-Saulnier responded with the 1927
159:
The MS.222 climbed faster than the MS.221 but was still slow at altitude, so a further aerodynamic clean-up in 1930 replaced the cross-axle undercarriage inherited from the MS.121 with a split-axle design, resulting in the MS.223 which first flew in April 1930.
144:
The precise date of the MS.221's first flight, flown by
Fronval, is not known but it was before March 1928. Despite being lighter and more powerful, it was significantly slower at altitude than its competitors, so one MS.221 prototype was re-engined with a
112:, built in 1928 to compete for a government contract in the "Jockey" (light fighter) programme. Two were built, one of which was progressively modified to increase its speed, but in 1930 the light fighter concept was abandoned.
133:. This proved to be underpowered and was superseded by the MS.221, which used the same basic airframe and armament with a 30% power increase, provided by a 450 kW (600 hp)
286:
In place of the cross-axle and its support, the MS.223 had simpler longitudinal V-struts, and each wheel had a vertical shock absorber leg to a reinforced forward wing strut.
693:
233:
and could be dropped in an emergency. Behind, the fuselage was of mixed construction; the forward main frames were metal but the structure further aft had wooden
229:
with piston heads exposed for cooling. The fighter's 265 L (58 imp gal; 70 US gal) fuel tank was separated from the engine by a
163:
By this time the failure of the "Jockey" programme was apparent and Morane-Saulnier turned their attention back to heavier, more traditional fighters.
36:
1788:
1798:
686:
662:
1783:
679:
501:
424:
267 km/h (166 mph, 144 kn) at 3,650 m (11,980 ft), 288 km/h (179 mph; 156 kn) at sea level
1740:
1613:
1608:
1603:
1598:
275:
was quadrantal in profile and carried an unbalanced rudder that reached down to the keel, moving in a gap between the elevators.
222:
of two inverted V-struts, one to each spar. Two almost parallel struts braced the wing at about 55% span to the lower fuselage.
1793:
1720:
1638:
319:
1735:
1653:
1643:
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1663:
1710:
1668:
195:
601:
546:
218:-increasing flaps for landing. The joint between the two panels was supported over the central fuselage on a
1761:
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767:
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215:
214:; as well as the normal, differential action for lateral control they could be operated together as
973:
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191:
149:
134:
226:
109:
53:
702:
265:
78:
464:
2×7.7 mm (0.303 in) Vickers or Darne machine guns, provided with 700 rounds.
17:
1777:
524:
400:
211:
138:
579:
396:
279:
264:, mounted at mid-fuselage and swept in plan, was in-flight adjustable, with split,
219:
199:
152:
Jupiter which could deliver full power at 3,800 m (12,500 ft). The wing
225:
The
Jupiter engines used were similarly installed on all variants under a dished
403:, 450 kW (600 hp) with full boost at 3,800 m (12,500 ft)
634:
245:
shaping its fabric covered, polygonal section. The front of the single, open
261:
184:
671:
156:
were also revised to reduce drag. It was then re-designated as the MS.222.
234:
207:
246:
203:
172:
238:
121:
68:
318:
153:
260:
The tail surfaces had dural frames and were fabric covered. The
675:
323:
Morane-Saulnier MS.221 3-view drawing from L'Air April 1, 1928
249:
was under the trailing edge behind a pair of fuselage-mounted
179:
out to semi-circular tips and mounted with 7° of sweep but no
625:
Bruner, Georges (1977). "Fighters a la
Francaise, Part One".
304:
One MS.221 re-engined with supercharger and modified struts.
409:
2-bladed, 2.85 m (9 ft 4 in) diameter wooden
125:
271:
which were narrow and had constant chord. The fighter's
1746:
Rallye, Rallye Club, Super Rallye and Rallye
Commodore
386:
265 L (58 imp gal; 70 US gal)
1677:
926:
710:
657:] (in French). Outreau, France: Lela Presse.
496:. Godalming, UK: Salamander Books. p. 416.
283:steerable tailskids to assist ground handling.
310:MS.222 with cleaner, split-axle undercarriage.
687:
649:Lacaze, Henri & Lherbert, Claude (2013).
8:
655:Morane Saulnier: Their Aircraft and Projects
492:Green, William; Swanborough, Gordon (1994).
694:
680:
672:
430:1,125 km (699 mi, 607 nmi)
175:wing was in two parts, each with constant
573:
571:
569:
567:
565:
563:
487:
485:
483:
481:
479:
477:
651:Morane Saulnier: ses avions, ses projets
519:
517:
515:
513:
448:12 min to 7,000 m (23,000 ft)
330:Les Ailes, June 1929 except where noted.
595:
593:
540:
538:
473:
442:12,000 m (39,000 ft) absolute
26:
278:The MS.221 and 222 had similar fixed
7:
1711:Épervier, Épervier II and Super 1500
141:. Two MS.221 prototypes were built.
257:firing through the propeller disc.
356:9.80 m (32 ft 2 in)
350:6.50 m (21 ft 4 in)
25:
580:"Le "Jockey" Morane-saulnier 222"
362:2.98 m (9 ft 9 in)
600:Bruno Parmentier (5 June 1999).
545:Bruno Parmentier (5 June 1999).
35:
1789:Single-engined tractor aircraft
368:16 m (170 sq ft)
578:Frachet, André (6 June 1929).
1:
1799:1920s French fighter aircraft
494:The Complete Book of Fighters
380:1,255 kg (2,767 lb)
202:which was strengthened with
374:947 kg (2,088 lb)
1815:
531:(106): 73, 75. March 1928.
43:
34:
29:
1784:Morane-Saulnier aircraft
602:"Morane-Saulnier MS-222"
547:"Morane-Saulnier MS-223"
525:"Le Morane-Saulnier 221"
335:General characteristics
315:Specifications (MS.222)
120:In the late 1920s both
324:
137:Jupiter nine-cylinder
106:Morane-Saulnier MS.221
18:Morane-Saulnier MS.223
1794:Parasol-wing aircraft
1736:Paris and Super Paris
1700:Comté de Nice or Nice
322:
210:occupied the entire
183:. Each part had two
1678:Names and nicknames
711:Designation letters
927:Numerical sequence
883:AN/ANB/ANR/ANL/ANS
397:turbo-supercharged
325:
255:Darne machine guns
147:turbo-supercharged
52:Single seat light
1771:
1770:
664:978-2-914017-70-1
446:Time to altitude:
237:and frames, with
102:
101:
16:(Redirected from
1806:
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440:Service ceiling:
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110:fighter aircraft
95:
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57:Type of aircraft
54:fighter aircraft
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703:Morane-Saulnier
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643:Further reading
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394:Gnome-Rhône 9As
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206:. Narrow-chord
198:apart from the
169:
150:Gnome-Rhône 9As
135:Gnome-Rhône 9Ae
118:
93:
79:Morane-Saulnier
64:National origin
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503:1-85833-777-1
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654:
650:
629:(3): 85–95.
626:
619:Bibliography
607:12 September
605:. Retrieved
583:
552:12 September
550:. Retrieved
528:
493:
461:
453:
451:
445:
439:
433:
427:
421:
414:
412:
406:
389:
383:
377:
371:
365:
359:
353:
347:
341:
334:
332:
327:
326:
285:
280:landing gear
277:
259:
224:
200:leading edge
170:
162:
158:
143:
119:
105:
103:
94:Number built
415:Performance
407:Propellers:
399:9-cylinder
390:Powerplant:
190:and wooden
116:Development
88:Early 1928
1778:Categories
1762:Versailles
1731:Monococque
469:References
434:Endurance:
366:Wing area:
298:Two built.
266:unbalanced
1764:(project)
1753:(project)
1751:Statodyne
1702:(project)
635:0143-5450
586:(416): 3.
584:Les Ailes
354:Wingspan:
328:Data from
269:elevators
262:tailplane
243:stringers
235:longerons
185:duralumin
705:aircraft
454:Armament
290:Variants
231:firewall
208:ailerons
194:and was
181:dihedral
124:and the
1757:Vanneau
1726:Lévrier
1721:Fleuret
1716:Fantôme
1706:Criquet
1669:MS.1500
1664:MS.1001
1289:MoS.149
1284:MoS.148
1279:MoS.147
1274:MoS.141
1269:MoS.140
1264:MoS.139
1259:MoS.138
1254:MoS.137
1249:MoS.136
1244:MoS.134
1239:MoS.133
1234:MoS.132
1229:MoS.131
1224:MoS.130
1219:MoS.129
1214:MoS.121
1209:MoS.120
360:Height:
348:Length:
251:Vickers
247:cockpit
239:formers
227:cowling
204:plywood
173:parasol
44:MS.222
30:MS.221
1741:Pétrel
1695:Bullet
1685:Alcyon
1659:MS.880
1654:MS.860
1649:MS.785
1644:MS.760
1639:MS.755
1634:MS.733
1629:MS.732
1624:MS.731
1619:MS.730
1614:MS.704
1609:MS.703
1604:MS.701
1599:MS.700
1594:MS.631
1589:MS.630
1584:MS.603
1579:MS.570
1574:MS.560
1569:MS.506
1564:MS.505
1559:MS.504
1554:MS.502
1549:MS.501
1544:MS.500
1539:MS.479
1534:MS.477
1529:MS.476
1524:MS.475
1519:MS.470
1514:MS.474
1509:MS.472
1504:MS.470
1499:MS.450
1494:MS.435
1489:MS.433
1484:MS.430
1479:MS.411
1474:MS.410
1469:MS.408
1464:MS.406
1459:MS.405
1454:MS.350
1449:MS.345
1444:MS.343
1439:MS.342
1434:MS.341
1429:MS.340
1424:MS.325
1419:MS.317
1414:MS.316
1409:MS.315
1404:MS.302
1399:MS.301
1394:MS.300
1389:MS.278
1384:MS.275
1379:MS.260
1374:MS.251
1369:MS.250
1364:MS.230
1359:MS.229
1354:MS.227
1349:MS.226
1344:MS.225
1339:MS.224
1334:MS.223
1329:MS.222
1324:MS.221
1319:MS.200
1314:MS.185
1309:MS.181
1304:MS.180
1299:MS.160
1294:MS.152
1204:MoS.60
1199:MoS.56
1194:MoS.53
1189:MoS.52
1184:MoS.51
1179:MoS.50
1174:MoS.49
1169:MoS.48
1164:MoS.47
1159:MoS.46
1154:MoS.45
1149:MoS.44
1144:MoS.43
1139:MoS.42
1134:MoS.41
1129:MoS.40
1124:MoS.39
1119:MoS.38
1114:MoS.37
1109:MoS.36
1104:MoS.35
1099:MoS.34
1094:MoS.33
1089:MoS.32
1084:MoS.31
1079:MoS.30
1074:MoS.29
1069:MoS.28
1064:MoS.27
1059:MoS.26
1054:MoS.25
1049:MoS.24
1044:MoS.23
1039:MoS.22
1034:MoS.21
1029:MoS.20
1024:MoS.19
1019:MoS.18
1014:MoS.17
1009:MoS.16
1004:MoS.15
999:MoS.14
994:MoS.13
989:MoS.12
984:MoS.11
979:MoS.10
661:
633:
500:
428:Range:
401:radial
307:MS.223
301:MS.222
295:MS.221
220:cabane
216:camber
167:Design
154:struts
131:MS.121
122:France
69:France
1690:Borel
974:MoS.9
969:MoS.8
964:MoS.7
959:MoS.6
954:MoS.5
949:MoS.4
944:MoS.3
939:MoS.2
934:MoS.1
653:[
462:Guns:
342:Crew:
188:spars
177:chord
49:Role
659:ISBN
631:ISSN
609:2017
554:2017
498:ISBN
436:5 hr
392:1 ×
241:and
192:ribs
171:The
104:The
873:AFH
828:TRK
344:One
273:fin
253:or
1780::
918:BH
913:BB
908:AV
903:AU
898:AT
893:AS
888:AR
878:AI
868:AF
863:AE
858:AC
843:WR
798:Nm
783:LH
778:LA
748:GB
743:GA
592:^
582:.
562:^
537:^
527:.
512:^
476:^
126:UK
98:2
853:Y
848:X
838:V
833:U
823:T
818:S
813:Q
808:P
803:O
793:N
788:M
773:L
768:K
763:J
758:I
753:H
738:G
733:F
728:C
723:B
718:A
695:e
688:t
681:v
667:.
637:.
611:.
556:.
506:.
20:)
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