531:
29:
475:, or a similar weapon, firing through the propeller boss. A reduction gear equipped power-plant with a resultant clockwise rotation propeller like the 8B, produced 160 kW (220 hp) at 2,100 rpm. Two known weapons fitted were the SAMC with a rifled barrel and a smooth-bore cannon firing canister ammunition. The moteur-canon could fire a single shot at a time through the hollow drive shaft without propeller interference. This cannon mount required an "elevated"
523:
337:
179:-driven tower shaft coming up from the crankcase along the rear end of each cylinder bank, with the final drive for each cylinder bank's camshaft accommodated within a semicircular bulge at the rear end of each valve cover. Aluminium parts were coated in vitreous enamel to reduce leakage. All parts subject to wear, and those critical for engine ignition were duplicated:
217:
development at this time. Rotary engines of increased power generally had increased weight, which in turn increased the already serious gyroscopic torque generated by the engine's rotation. A further increase in torque was considered unacceptable, and the power to weight ratio of the new rotary engines under development did not appeal to aircraft designers.
129:
Hispano-Suiza 8 engines and variants produced by
Hispano-Suiza and other companies under licence were built in twenty-one factories in Spain, France, Britain, Italy, and the U.S. Derivatives of the engine were also used abroad to power numerous aircraft types and the engine can be considered as the
216:
on July 21, 1915, and tested for 50 hours, succeeding against all expectations. The design also promised far more development-potential than rotary engines. This was despite being the most common type, then in use, for most aircraft. Also, rotary engines were getting close to the limits of their
211:
rotary 130 hp (97 kW), 173 kg (381 lb). The new engine was presented to the French
Ministry of War in February 1915, and tested for 15 hours at full power. This was standard procedure for a new engine design to be admitted into military service. However, because of lobbying by
166:
The first 8A kept the standard configuration of
Birkigt's existing design: eight cylinders in 90° Vee configuration, a displacement of 11.76 litres (717.8 cu in) and a power output of 140 hp at 1,900 rpm. In spite of the similarities with the original design, the engine had been
284:
110 kW (150 hp) at 2000 rpm, entered production in July 1915. Early HS-8A engines were plagued with various problems which required further work and was the standard powerplant for early-production SPAD VIIs and the
Curtiss "Jenny"
560:
was a bored out version of the 8B, intended for use in bombers, with a displacement of 18.5 L (1,128.94 cu in). Despite the increased weight of 564 lb (256 kg), the 8F was also installed in fighters such as the
425:, and (d) several other Allied aircraft types, with its gear reduction easily identifiable in vintage World War I photos, from its use of a clockwise (viewed from in front, otherwise known as a left hand tractor) rotation propeller.
649:
150 kW (200 hp), compression ratio of 5.3 :1. Wolseley's engineers removed problems with the crankshaft and increased the compression ratio to give more power, with some early engines having a compression ratio of
1788:"Los motores V8 de aviación de La Hispano Suiza (1914–1918)" by Jacinto García Barbero (Edited by Asociación de Amigos del Museo Del Aire, Museo de Aeronáutica y Astronáutica, CECAF. Depósito legal: M-41737-2005) 219 pages.
388:
150 kW (200 hp), compression ratio of 4.8:1, reduction gear 0.75:1. However the reduction gear system was fragile, and often broke down, sometimes with spectacular results ending up with the entire propeller,
202:
of equivalent power. This empty weight does not include the radiator and coolant fluid. Generally, air-cooled engines are lighter than their equivalent horsepower water-cooled counterparts. For example, the
212:
French engine manufacturers, the
Spanish-made engine was ordered to undergo a bench test that no French-made engine had yet passed: a 50-hour run at full speed. The HS-31 was therefore sent back to
175:
cylinder heads. The inlet and exhaust ports were cast into the blocks, the valve seats were in the top face of the steel cylinder liners, which were screwed into the blocks. Using a rotating
1638:
220:
French officials ordered production of the 8A to be started as soon as possible and issued a requirement for a new single-seat high-performance fighter aircraft using the new engine. The
163:
led work on an aircraft engine based on his successful V8 automobile engine. The resulting engine, called the
Hispano-Suiza 8A (HS-31), made its first appearance in February 1915.
393:
and driven gear parting company from the airframe. Progressive refinement of the engine brought the available power to 175 kW (235 hp) by the end of 1917.
259:, but military designations used the conventional system of Hispano-Suiza(engine manufacturer) 8(no of cylinders) A(engine series) b(variant) r(attribute), thus
627:
472:
1846:
1874:
1747:
1758:
Janes
Fighting Aircraft of World War I by Michael John Haddrick Taylor (Random House Group Ltd. 20 Vauxhall Bridge Road, London SW1V 2SA, 2001,
1647:
289:
variants. The demand for the
Hispano-Suiza engine was such that other manufacturers began producing it under licence, in France, Great Britain (
1664:
198:
were major problems in early aviation. The engine and its accessories weighed 185 kg (408 lb), making it 40% lighter than a
1973:
1839:
1968:
167:
substantially refined. The crankshaft was machined from a solid piece of steel. The cylinder blocks were cast aluminium and of
1404:
616:(1926) 140 mm × 150 mm (5.5 in × 5.9 in) bore x stroke, 260 kW (350 hp) for take-off.
332:(1929) 120 mm × 130 mm (4.7 in × 5.1 in) bore x stroke, 160 kW (210 hp) for take-off.
315:
from 4.7 to 5.3, Birkigt was able to increase the power output . The 8Ab began replacing the 8Aa on SPAD VIIs in early 1917.
573:. Engine speed being lower than that of the HS-8B, the reduction gear was deleted, thereby increasing engine reliability.
1393:
A Hispano-Suiza 8Aa Type 34, made in 1916, is on public display at Museo de Aeronáutica y Astronáutica at Madrid, Spain.
1832:
98:
1814:
680:
150 kW (200 hp), compression ratio of 4.7 :1, reduction spur gear to 0.593:1. With stronger crankshaft webs.
1763:
1619:
1020:
700:
4-cyl in-line water-cooled 56 kW (75 hp) 120 mm × 130 mm (4.7 in × 5.1 in)
688:
150 kW (200 hp), compression ratio of 4.7 :1, reduction spur gear to 0.593:1. With balanced crankshafts.
410:
1168:
1397:
515:
Cannon-equipped 160 kW (220 hp) at 2,100 rpm with 5.3:1 compression. Given the company designation
506:
Cannon-equipped 160 kW (220 hp) at 2,000 rpm with 4.7:1 compression. Given the company designation
497:
Cannon-equipped 168 kW (225 hp) at 2,100 rpm with 5.3:1 compression. Given the company designation
1016:
1600:
One prototype of this aircraft engine is preserved in the "Museo de Aeronáutica y Astronáutica" in Madrid.
1689:
526:
Hispano Suiza 8Ca. The large shafts that drove the valves are visible at the back of the cylinder banks.
1010:
270:
100 kW (140 hp), initial production and test engines, with few applications, including early
1818:
1131:
378:
150 kW (200 hp) at 2,300 rpm, low compression ratio of 4.7:1, spur geared at 0.585:1.
1569:
479:
design, bringing the intake "runners" straight off the inner surfaces of the cylinder banks to the
1668:
114:
in 1914 that went on to become the most commonly used liquid-cooled engine in the aircraft of the
683:
634:
694:
Wright-Martin built Type 34/HS8Aa 150 hp (112 kW) at 1,400 rpm and 4.72:1 compression.
1163:
1004:
998:
986:
925:
675:
655:
621:
562:
159:
automobile and engine company were switched to the production of war materiel. Chief engineer
1947:
665:
195:
1866:
47:
8:
1808:
1452:
886:
810:
644:
1731:
626:
110 kW (150 hp), compression ratio of 4.7:1. License production of the 8Aa at
1919:
1914:
1771:
1116:
832:
670:
150 kW (200 hp), compression ratio of 4.7 :1, reduction spur gear to 0.593:1.
566:
480:
221:
1929:
1924:
1909:
1904:
1899:
1894:
1889:
1759:
1615:
1101:
556:
220 kW (300 hp) at 2,100 rpm (eq. 750 lb·ft torque). The direct drive
312:
298:
131:
869:
301:
in Turin) and Russia. Total production of the HS-8Aa amounted to some 6,000 engines.
1121:
605:
286:
188:
1858:
1824:
1803:
1646:(in French). Boix-Colombes: Société Française Hispano-Suiza. 1932. Archived from
1534:
1443:
1136:
1106:
1091:
1030:
837:
570:
476:
422:
294:
229:
207:
rotary put out 230 hp (170 kW) and weighed 220 kg (490 lb),
1540:
1186:
1181:
1024:
980:
898:
484:
290:
213:
138:
V12 derivative aero-engines) which was in service during the Second World War.
115:
85:
1798:
444:
160 kW (220 hp), compression ratio of 5.3:1, reduction gear 0.75:1.
1962:
1884:
1855:
1434:
940:
935:
880:
461:
160 kW (220 hp), compression ratio of 5.3:1, reduction gear 0.75:1.
434:
160 kW (220 hp), compression ratio of 5.3:1, reduction gear 0.75:1.
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160:
962:
350:
150 kW (200 hp), compression ratio 5.3:1, geared at 0.75:1. The
122:
was rated at 140 hp (100 kW) and the later, larger displacement
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1799:
Old
Rhinebeck Aerodrome's Hispano-Suiza V8 powered Curtiss JN-4H Jenny
1537:, a single bank of the Hispano-Suiza, on an Australian-made crankcase.
1690:
http://www.flightglobal.com/pdfarchive/view/1919/1919%20-%200199.html
1427:
1078:
1048:
718:
130 kW (180 hp) at 1,700 rpm and 5.33:1 compression(HC 'I')
355:
152:
101:
44:
522:
336:
228:
was the result of this requirement and allowed the Allies to regain
1939:
1819:
Moteurs d'Aviation
License Hispano-Suiza (Compagnie de Fives-Lille)
1111:
1072:
225:
1146:
602:
569:, and would have powered the never-produced Mk.II version of the
130:
ancestor of another successful engine by the same designer, the
135:
1587:
Browne, T.C. "Retrospect: 1924 Hispano-Suiza H6c Speedster",
151:
At the beginning of World War I, the production lines of the
311:
130 kW (180 hp) at 2,100 rpm, increasing the
172:
104:
1821:, engine manual (types 150 hp, 180 hp, 200 hp and 220 hp)
1813:
Hispano-Suiza 8Aa at Museo de Aeronáutica y Astronáutica.
639:
130 kW (180 hp), compression ratio of 5.3 :1.
1410:
736:
220 kW (300 hp), based on the Type 42/HS8F
409:
were used (a) to power the earliest versions of the
249:
Hispano-Suiza company type numbers were prefixed by
471:The 8Be fitted with the 37 mm (1.457 in)
1854:
1152:
1960:
1171:(ハンザ式水上偵察機, Type Hansa Surveillance Floatplane)
712:150 kW (200 hp) geared A with cannon
1614:. Marlborough, Wiltshire: Airlife Publishing.
1403:A Wright-Hisso 8A is on public display at the
1396:A Wright-Hisso 8A is on public display at the
1840:
1023:(8B, 8Ba or 8Bb on earliest versions and the
660:160 kW (210 hp) at 2,000 rpm.
593:, compression ratio of 5.3:1, direct drive.
1847:
1833:
1417:
608:racer developing 280 kW (380 hp)
243:British Piston Engines and their Aircraft
1612:British Piston Engines and their Aircraft
141:
118:during the First World War. The original
36:Preserved "direct-drive" Hispano-Suiza 8
1769:
1725:
1723:
1721:
529:
521:
421:, (c) front-line active versions of the
335:
1719:
1717:
1715:
1713:
1711:
1709:
1707:
1705:
1703:
1701:
1609:
1961:
1633:
1631:
1603:
1488:1 Claudel or Zenith updraft carburetor
1828:
1729:
1405:National Museum of the U.S. Air Force
1387:
1736:. Dayton, Ohio: THE OTTERBEIN PRESS.
1698:
1192:
171:type that is, in one piece with the
1628:
1085:
706:150 kW (200 hp) geared A
293:), Italy (Nagliati in Florence and
126:reached 330 hp (250 kW).
13:
1770:Hartmann, Gérard (December 2005).
358:firing through the propeller boss.
14:
1985:
1792:
1411:Specifications (Hispano-Suiza 8a)
1640:Moteurs d'Aviation Hispano-Suiza
27:
1782:
1665:"V-8, Hispano-Suiza Model 8 Ca"
804:
589:220 kW (300 hp), aka
1974:Hispano-Suiza aircraft engines
1777:(in French). pp. 6 pages.
1740:
1683:
1657:
1594:
1581:
1519:18.2 g/(kW•h) (0.03 lb/(hp•h))
1498:
1398:Aerospace Museum of California
1:
1969:1910s aircraft piston engines
1575:
1513:310 g/(kW•h) (0.51 lb/(hp•h))
1470:
487:. The engine was used on the
1733:Airplane Engine Encyclopedia
1507:150 hp (112 kW) at 1,700 rpm
1169:Hanza-shiki suijō teisatsuki
1017:Royal Aircraft Factory S.E.5
793:A 220 kW (300 hp)
784:Wright-Hisso 300 hp V-8
778:Wright-Hisso 220 hp V-8
772:Wright-Hisso 180 hp V-8
581:generally similar to the 8F.
187:reliability, valve springs,
7:
1523:
1132:Naval Aircraft Factory TS-3
1027:derivative on later models)
235:
10:
1990:
1482:SOHC (single overhead cam)
1069:-1 (post-war modification)
1011:Nieuport-Delage Sesquiplan
753:H with 37mm Baldwin cannon
146:
16:V-8 piston aircraft engine
1938:
1865:
1809:Pilot Friend Aero Engines
1466:202 kg (445 lb)
1426:8-cylinder liquid-cooled
1260:
1257:
1246:
1235:
1224:
35:
26:
21:
1730:Angle, Glenn D. (1921).
1570:List of aircraft engines
917:(8F) initial design only
797:produced copy of the 8Fb
764:experimental 300 hp
1748:"Hispano-Suiza Model A"
1695:February 13, 1919 p 199
1418:General characteristics
684:Wolseley W.4B Adder III
635:Wolseley W.4A Python II
194:Engine reliability and
1610:Lumsden, Alec (2003).
1164:Yokosuka Ro-go Ko-gata
1005:Nieuport-Delage NiD 38
999:Nieuport-Delage NiD 29
987:Martinsyde F.4 Buzzard
926:Gourdou-Leseurre GL.21
676:Wolseley W.4B Adder II
656:Wolseley W.4A Viper II
622:Wolseley W.4A Python I
563:Nieuport-Delage NiD 29
535:
527:
341:
255:or written in full as
196:power to weight ratios
142:Design and development
1772:"Le V8 Hispano-Suiza"
666:Wolseley W.4B Adder I
547:Hispano-Suiza Type 41
539:Hispano-Suiza Type 40
533:
525:
413:, (b) along with the
339:
257:Hispano-Suiza Type 31
1153:Mitsubishi "Hi"shiki
730:('D' without cannon)
628:Wolseley Motors Ltd.
473:SAMC Model 37 cannon
1529:Related development
1457:11.76 L (717.77 in)
1198:
887:Farman F.121 Jabiru
811:Austin-Ball A.F.B.1
645:Wolseley W.4A Viper
1547:Comparable engines
1388:Engines on display
1197:
1117:Dayton-Wright TW-3
1081:(single prototype)
833:Bernard SIMB AB 10
813:(single prototype)
800:Wright-Hisso V-720
567:Martinsyde Buzzard
536:
528:
481:updraft carburetor
368:Coupled 8B engines
354:was the 8B with a
342:
261:Hispano-Suiza 8Abr
232:over the Germans.
1956:
1955:
1511:Fuel consumption:
1448:130 mm (5.118 in)
1439:120 mm (4.724 in)
1385:
1384:
1346:Power output (hp)
1255:Compression ratio
1193:Comparative table
1102:Consolidated PT-1
959:& Let.3 (8Ba)
866:(rare subvariant)
534:Hispano Suiza 8Ca
340:Hispano-Suiza 8Be
313:compression ratio
299:SCAT (automobile)
132:Hispano-Suiza 12Y
91:
90:
1981:
1859:aircraft engines
1849:
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1835:
1826:
1825:
1804:Aviation History
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1667:. Archived from
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1601:
1598:
1592:
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1517:Oil consumption:
1244:Displacement (l)
1199:
1196:
1176:300 HP (8F)
1158:200 HP (8B)
1122:Huff-Daland TW-5
1086:Wright-Hispano E
1039:prototypes (8Ba)
756:Wright-Hisso K-2
739:Wright-Hisso H-2
721:Wright-Hisso E-2
606:Schneider Trophy
124:Hispano-Suiza 8F
120:Hispano-Suiza 8A
74:
31:
22:Hispano-Suiza 8
19:
18:
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1492:Cooling system:
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1137:Travel Air 3000
1107:Cox-Klemin TW-2
1088:
1031:Sopwith Dolphin
838:Blanchard Brd.1
807:
571:Sopwith Dolphin
477:intake manifold
423:Sopwith Dolphin
365:8B twin (HS-39)
241:Some data from:
238:
230:air superiority
222:Louis Béchereau
149:
144:
95:Hispano-Suiza 8
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1867:Piston engines
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1793:External links
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1671:on 7 June 2010
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504:
501:
495:
492:
485:plenum chamber
469:
463:
462:
459:
453:
452:
451:
450:
442:
436:
435:
432:
395:
394:
386:
380:
379:
376:
370:
369:
366:
360:
359:
348:
334:
333:
330:
324:
323:
321:
317:
316:
309:
303:
302:
291:Wolseley Adder
282:
276:
275:
268:
237:
234:
214:Chalais-Meudon
148:
145:
143:
140:
116:Entente Powers
110:introduced by
89:
88:
86:Wolseley Viper
83:
79:
78:
75:
69:
68:
65:
61:
60:
55:
51:
50:
42:
38:
37:
33:
32:
24:
23:
15:
9:
6:
4:
3:
2:
1986:
1975:
1972:
1970:
1967:
1966:
1964:
1949:
1946:
1945:
1943:
1941:
1937:
1931:
1928:
1926:
1923:
1921:
1918:
1916:
1913:
1911:
1908:
1906:
1903:
1901:
1898:
1896:
1893:
1891:
1888:
1886:
1883:
1881:
1878:
1876:
1873:
1872:
1870:
1868:
1864:
1860:
1857:
1856:Hispano-Suiza
1850:
1845:
1843:
1838:
1836:
1831:
1830:
1827:
1820:
1817:
1815:
1812:
1810:
1807:
1805:
1802:
1800:
1797:
1796:
1787:
1786:
1773:
1768:
1765:
1764:1-85170-347-0
1761:
1757:
1756:
1749:
1743:
1735:
1734:
1726:
1724:
1722:
1720:
1718:
1716:
1714:
1712:
1710:
1708:
1706:
1704:
1702:
1694:
1691:
1686:
1670:
1666:
1660:
1649:
1642:
1641:
1634:
1632:
1623:
1621:1-85310-294-6
1617:
1613:
1606:
1597:
1590:
1584:
1580:
1571:
1568:
1567:
1566:
1565:
1564:Related lists
1559:
1556:
1554:
1551:
1550:
1549:
1548:
1542:
1539:
1536:
1533:
1532:
1531:
1530:
1518:
1515:
1512:
1509:
1506:
1505:Power output:
1503:
1502:
1493:
1490:
1487:
1484:
1481:
1479:
1475:
1474:
1465:
1463:
1459:
1456:
1454:
1450:
1447:
1445:
1441:
1438:
1436:
1432:
1430:piston engine
1429:
1425:
1422:
1421:
1415:
1406:
1402:
1399:
1395:
1392:
1391:
1380:
1377:
1374:
1371:
1368:
1365:
1364:
1360:
1357:
1354:
1351:
1348:
1345:
1344:
1340:
1337:
1334:
1331:
1328:
1325:
1324:
1320:
1317:
1314:
1311:
1308:
1305:
1304:
1300:
1297:
1294:
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1288:
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1284:
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1268:
1265:
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1254:
1253:
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1238:
1232:
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1227:
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1220:
1216:
1213:
1210:
1207:
1204:
1201:
1200:
1188:
1185:
1183:
1180:
1179:
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1174:
1170:
1167:
1165:
1162:
1161:
1157:
1156:
1148:
1145:
1143:
1140:
1138:
1135:
1133:
1130:
1128:
1125:
1123:
1120:
1118:
1115:
1113:
1110:
1108:
1105:
1103:
1100:
1098:
1095:
1093:
1090:
1089:
1080:
1077:
1074:
1071:
1068:
1065:
1062:
1059:
1056:
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1050:
1047:
1044:
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1038:
1035:
1032:
1029:
1026:
1022:
1018:
1015:
1012:
1009:
1006:
1003:
1000:
997:
994:
991:
988:
985:
982:
979:
976:
973:
970:
967:
964:
961:
958:
955:
952:
949:
947:
944:
942:
941:Hanriot HD.20
939:
937:
936:Hanriot HD.15
934:
932:
929:
927:
924:
922:
919:
916:
913:
910:
907:
905:
902:
900:
897:
894:
891:
888:
885:
882:
881:Dewoitine D.1
879:
876:
873:
871:
868:
865:
861:
858:
855:
852:
850:
847:
844:
841:
839:
836:
834:
831:
829:
826:
824:
821:
818:
815:
812:
809:
808:
799:
796:
792:
789:
786:
783:
780:
777:
774:
771:
769:
766:
763:
760:
758:
755:
752:
749:
747:
744:
741:
738:
735:
732:
729:
726:
723:
720:
717:
714:
711:
708:
705:
702:
699:
696:
693:
690:
687:
685:
682:
679:
677:
674:
673:
669:
667:
664:
663:
659:
657:
654:
653:
648:
646:
643:
642:
638:
636:
633:
632:
629:
625:
623:
620:
619:
615:
613:8Fe (HS-42VS)
612:
611:
607:
604:
600:
597:
596:
592:
588:
585:
584:
580:
577:
576:
572:
568:
564:
559:
555:
552:
549:
546:
545:
541:
538:
537:
532:
524:
518:
514:
511:
509:
505:
502:
500:
496:
493:
490:
486:
482:
478:
474:
470:
467:
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465:
460:
457:
456:
455:
449:
446:
445:
443:
440:
439:
438:
433:
430:
429:
428:
426:
424:
420:
416:
412:
408:
404:
400:
392:
387:
384:
383:
382:
377:
374:
373:
372:
367:
364:
363:
362:
357:
353:
349:
346:
345:
344:
338:
331:
328:
327:
326:
322:
319:
318:
314:
310:
307:
306:
305:
300:
296:
292:
288:
283:
280:
279:
278:
273:
269:
266:
265:
264:
262:
258:
254:
253:
248:
244:
242:
233:
231:
227:
223:
218:
215:
210:
206:
201:
200:rotary engine
197:
192:
190:
186:
185:dual ignition
182:
178:
174:
170:
164:
162:
158:
157:Hispano-Suiza
154:
139:
137:
133:
127:
125:
121:
117:
113:
112:Hispano-Suiza
109:
106:
103:
100:
96:
87:
84:
81:
80:
76:
71:
70:
66:
63:
62:
59:
58:Hispano-Suiza
56:
54:Manufacturer
53:
52:
49:
48:piston engine
46:
43:
40:
39:
34:
30:
25:
20:
1879:
1783:Bibliography
1742:
1732:
1692:
1685:
1673:. Retrieved
1669:the original
1659:
1648:the original
1639:
1611:
1605:
1596:
1588:
1583:
1563:
1562:
1558:Sunbeam Arab
1546:
1545:
1528:
1527:
1516:
1510:
1504:
1491:
1486:Fuel system:
1485:
1476:
1460:
1453:Displacement
1451:
1442:
1433:
1423:
1414:
1112:Curtiss AT-4
957:Letord Let.2
951:Letord Let.1
931:Hanriot HD.5
921:Fokker S.III
915:Fokker D.XII
863:
860:Curtiss JN-4
854:Caudron C.61
849:Caudron C.59
843:Caudron R.11
805:Applications
795:Soviet Union
787:geared drive
781:geared drive
775:direct drive
742:improved 'H'
590:
557:
516:
507:
498:
468:8BeC (HS-38)
464:
454:
447:
437:
427:
414:
406:
402:
398:
396:
381:
371:
361:
351:
343:
325:
304:
277:
272:Nieuport 14s
260:
256:
251:
250:
246:
245:
240:
239:
219:
205:Bentley BR.2
193:
165:
161:Marc Birkigt
150:
134:(and Soviet
128:
123:
119:
99:water-cooled
94:
92:
73:Number built
1766:), page 289
1589:Motor Trend
1553:Peugeot 8Aa
1499:Performance
1233:Stroke (mm)
1142:Vought VE-7
1127:Loening M-8
1092:Boeing NB-2
1061:SPAD S.XIII
1037:Sopwith B.1
993:Nieuport 14
946:Itoh Emi 29
904:Fokker D.IX
875:Descamps 27
828:Bartel BM-5
819:(from 1925)
598:8Fd Special
550:(8A ?)
542:(8E ?)
419:SPAD S.XIII
308:8Ab (HS-34)
281:8Aa (HS-31)
181:spark plugs
108:aero engine
1963:Categories
1675:24 October
1576:References
1478:Valvetrain
1471:Components
1462:Dry weight
1326:Weight(kg)
1306:Height (m)
1266:Length (m)
1067:Standard J
1055:SPAD S.XII
1043:SPAD S.VII
1019:(8Aa) and
975:Letov Š-14
969:Letov Š-13
909:Fokker D.X
893:FBA Type H
823:Avia BH-22
817:Avia BH-21
591:HS Type 42
553:8F (HS-42)
517:HS Type 44
508:HS Type 44
499:HS Type 38
489:SPAD S.XII
391:driveshaft
347:8B (HS-35)
224:-designed
209:Clerget 9B
177:bevel gear
64:First run
1940:Turbojets
1286:Width (m)
1222:Bore (mm)
1079:Wibault 1
1049:SPAD S.XI
963:Letov Š-7
356:Lewis gun
267:8 (HS-31)
153:Barcelona
82:Variants
1524:See also
1366:at (rpm)
1147:Waco DSO
1073:Waco DSO
724:(HC 'E')
601:For the
236:Variants
226:SPAD VII
189:magnetos
169:monobloc
1358:200/235
603:CAMS 38
512:8Cc/220
503:8Cb/180
494:8Ca/220
191:, etc.
147:Origins
77:49,800
1948:Verdon
1762:
1693:Flight
1618:
1494:liquid
1444:Stroke
1250:18.47
1202:Model
1021:S.E.5a
845:(8Bba)
650:5.6:1.
417:, the
411:S.E.5a
155:based
136:Klimov
1775:(PDF)
1651:(PDF)
1644:(PDF)
1424:Type:
1381:2100
1321:0.88
1301:0.89
1281:1.32
1247:11.76
1063:(8Be)
1057:(8Cb)
1051:(8Be)
1013:(8Fb)
1007:(8Ab)
1001:(8Fb)
989:(8Fb)
983:(8Ab)
977:(8Fb)
971:(8Fb)
965:(8Fb)
911:(8Fb)
895:(8Aa)
889:(8Ac)
883:(8Fb)
877:(8Fb)
864:Jenny
856:(8Ac)
352:HS-36
295:Itala
287:JN-4H
247:Note:
97:is a
67:1914
41:Type
1920:14AB
1915:14AA
1760:ISBN
1677:2010
1616:ISBN
1435:Bore
1378:2300
1375:2100
1372:2000
1369:1900
1361:300
1341:256
1318:0.90
1315:0.87
1312:0.81
1309:0.77
1298:0.86
1295:0.85
1292:0.83
1289:0.81
1278:1.36
1275:1.31
1272:1.25
1269:1.19
1261:5.3
1239:150
1228:140
1211:8Ab
1208:8Aa
1097:AT-3
1075:(8a)
1045:(8A)
1033:(8B)
995:(8A)
953:(8A)
565:and
448:8Bda
405:and
397:The
183:for
173:SOHC
105:SOHC
93:The
1930:18S
1925:18R
1910:12Z
1905:12Y
1900:12X
1895:12N
1890:12M
1428:Vee
1355:180
1352:150
1349:140
1338:236
1335:230
1332:215
1329:195
1258:4.7
1236:130
1225:120
1217:8F
1214:8B
1205:8A
790:M-6
586:8Fb
578:8Fa
483:'s
458:8Be
441:8Bd
431:8Bc
415:8Bd
407:8Bb
403:8Ba
385:8Bb
375:8Ba
329:8Ad
320:8Ac
252:HS-
1965::
1885:9V
1700:^
1630:^
862:H
558:8F
401:,
399:8B
263:.
102:V8
45:V8
1880:8
1875:6
1848:e
1841:t
1834:v
1750:.
1679:.
1624:.
1480::
1464::
1455::
1446::
1437::
1400:.
491:.
297:/
274:.
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
