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SNCAC NC.150

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SNCAC began work on two prototypes as a private venture in 1938. These two prototypes were not to be fitted with cabin pressurisation, although this was planned for a third prototype. The French Air Ministry placed an order for the two prototypes on 24 April 1939, with the second aircraft to carry
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caused by shortages of light alloys, and after successful testing in early 1940, ordered a change of plans. Pressurisation was to be abandoned, and the unusual central supercharger with its dedicated engine (known as the
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in 1936, the new company inherited Farman's experience in high-altitude research, and this research continued. In 1937, it proposed a
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skinning. Similarly, the fuselage had wooden forward and aft fuselage section connecting to the metal centre section, while the
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French Aircraft 1939–1942: Fighters, Bombers, Reconnaissance and Observation types: Volume 2: From Dewoitine to Potez
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such as wood. The wings were of mixed construction, with a metal centre-section, and wood outer wings that had metal
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Third prototype, representing original bomber design, with pressure cabin and full armament. Not completed.
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SNCAC continued work on high-altitude aircraft, proposing two pressurised bombers in 1938. The first, the
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bomber, this being developed into the unpressurised NC.223.4 transport, of which three were built for
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on 11 May 1939. Meanwhile, the French Air Ministry had become worried about possible delays to the
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to Germany in June 1940, both the second and third prototypes being abandoned before completion.
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When the nationalisation of the French aircraft industry resulted in the creation of the
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twin-engined bombers which were planned to re-equip the medium bomber squadrons of the
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full armament. The first prototype, designated NC.150.01, made its maiden flight from
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War Planes of the Second World War: Volume Seven: Bombers and Reconnaissance Aircraft
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510 km/h (317 mph, 275 kn) at 8,000 m (26,250 ft) (long-range cruise)
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War Planes of the Second World War:Volume Seven Bombers and Reconnaissance Aircraft
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Second prototype. Unpressurised but to be fitted with full armament. Not completed.
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Planned production version powered by two supercharged Hispano-Suiza 12Y engines.
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liquid-cooled V12 engine driving NC-C2 supercharger, 510 kW (690 hp)
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was of wooden construction with plywood skinning. It was to be powered by two
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Planned production version powered by two supercharged 1,850 hp (1,380 kW)
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in June 1940 ended development with only the single example being built.
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Société Nationale de Constructions Aéronautiques du Centre (SNCAC)
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600 km/h (373 mph, 324 kn) at 8,000 m (26,250 ft)
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First prototype. Not fitted with pressurisation and unarmed.
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Société Nationale de Constructions Aéronautiques du Centre
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Specifications (NC.150 - armament planned for 150.02)
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Aircraft of comparable role, configuration, and era
97:designed and flown just prior to the start of the 89:(also known as the Centre NC.150) was a prototype 916: 580: 578: 576: 574: 572: 544: 542: 587: 560: 530: 500: 180:which was designed to make maximum use of non- 672: 406:2,200 km (1,367 mi, 1,188 nmi) 569: 551: 539: 509: 626:. Paris: Histoire & Collections, 2005. 679: 665: 596: 523: 521: 438:cannon in power operated dorsal mounting, 609:. Retrieved 5 September 2010. (In French) 124: 622:Breffort, Dominique and André Jouineau. 518: 917: 331:21.882 m (71 ft 9.5 in) 660: 249:Development was stopped, however, by 945:Twin piston-engined tractor aircraft 343:61.10 m (657.7 sq ft) 451:1 × machine gun in ventral mounting 337:4.19 m (13 ft 9 in) 325:17.60 m (57 ft 9 in) 13: 527:Breffort and Jouineau 2005, p. 79. 14: 956: 644: 418:19 min 7 s to 8,000 m (26,250 ft) 369:, 720 kW (960 hp) each 291:Pratt & Whitney R-2800 S1A4-G 215:engine mounted in the fuselage. 105:, with a third engine driving a 24: 355:10,077 kg (22,216 lb) 172:. The NC.150 was a mid-winged 412:11,380 m (37,350 ft) 349:7,733 kg (17,048 lb) 1: 616: 940:Aircraft first flown in 1939 925:1930s French bomber aircraft 7: 463: 293:Double Wasp radial engines. 256: 10: 961: 876: 695: 640:. London: Macdonald, 1967 459:1,200 kg (2,650 lb) bombs 23: 18: 593:Green 1967, pp. 155–156. 566:Green 1967, pp. 154–156. 536:Green 1967, pp. 153–154. 506:Green 1967, pp. 151–152. 493: 101:. It was a twin-engined 475:Lioré et Olivier LeO 45 363:Hispano-Suiza 12Y 32/33 310:General characteristics 225:Lioré et Olivier LeO 45 178:tailwheel undercarriage 111:Lioré et Olivier LeO 45 125:Design and development 211:driven by a separate 139:Farman Aviation Works 137:) from the merger of 448:machine gun in nose, 436:Hispano-Suiza HS.404 377:Hispano-Suiza 12Xirs 36:High-altitude bomber 603:"S.N.C.A.C. NC.150" 584:Green 1967, p. 156. 557:Green 1967, p. 155. 548:Green 1967, p. 153. 182:strategic materials 176:with a retractable 119:surrender of France 515:Green 1967, p.152. 251:France's surrender 153:derivative of the 935:Mid-wing aircraft 912: 911: 690:(Centre) aircraft 416:Time to altitude: 213:Hispano-Suiza 12X 202:Hispano-Suiza 12Y 83: 82: 952: 681: 674: 667: 658: 657: 636:Green, William. 610: 600: 594: 591: 585: 582: 567: 564: 558: 555: 549: 546: 537: 534: 528: 525: 516: 513: 507: 504: 426: 410:Service ceiling: 387: 312: 221:Toussus-le-Noble 99:Second World War 76: 46: 38:Type of aircraft 28: 16: 15: 960: 959: 955: 954: 953: 951: 950: 949: 915: 914: 913: 908: 872: 691: 685: 647: 619: 614: 613: 601: 597: 592: 588: 583: 570: 565: 561: 556: 552: 547: 540: 535: 531: 526: 519: 514: 510: 505: 501: 496: 466: 427: 422: 383: 308: 300: 259: 127: 95:bomber aircraft 74: 45:National origin 44: 39: 12: 11: 5: 958: 948: 947: 942: 937: 932: 930:SNCAC aircraft 927: 910: 909: 907: 906: 901: 896: 891: 886: 880: 878: 874: 873: 871: 870: 865: 860: 855: 850: 845: 840: 835: 830: 825: 820: 815: 810: 805: 800: 795: 790: 785: 780: 775: 770: 765: 760: 755: 750: 745: 740: 735: 730: 725: 720: 715: 710: 705: 699: 697: 693: 692: 684: 683: 676: 669: 661: 655: 654: 646: 645:External links 643: 642: 641: 634: 618: 615: 612: 611: 595: 586: 568: 559: 550: 538: 529: 517: 508: 498: 497: 495: 492: 489: 488: 485:Petlyakov Pe-8 482: 477: 465: 462: 461: 460: 454: 453: 452: 449: 420: 419: 413: 407: 401: 395: 392:Maximum speed: 381: 380: 370: 365:liquid-cooled 356: 350: 344: 338: 332: 326: 320: 299: 296: 295: 294: 287: 284: 281: 278: 275: 272: 269: 266: 263: 258: 255: 244:radial engines 234:Armée de l'Air 155:Farman F.223.3 149:transatlantic 126: 123: 93:high-altitude 81: 80: 77: 71: 70: 67: 63: 62: 57: 53: 52: 47: 41: 40: 37: 34: 30: 29: 21: 20: 9: 6: 4: 3: 2: 957: 946: 943: 941: 938: 936: 933: 931: 928: 926: 923: 922: 920: 905: 902: 900: 897: 895: 892: 890: 887: 885: 882: 881: 879: 875: 869: 866: 864: 861: 859: 856: 854: 851: 849: 846: 844: 841: 839: 836: 834: 831: 829: 826: 824: 821: 819: 816: 814: 811: 809: 806: 804: 801: 799: 796: 794: 791: 789: 786: 784: 781: 779: 776: 774: 771: 769: 766: 764: 761: 759: 756: 754: 751: 749: 746: 744: 741: 739: 736: 734: 731: 729: 726: 724: 721: 719: 716: 714: 711: 709: 706: 704: 701: 700: 698: 694: 689: 682: 677: 675: 670: 668: 663: 662: 659: 652: 649: 648: 639: 635: 633: 632:2-915239-49-5 629: 625: 621: 620: 608: 604: 599: 590: 581: 579: 577: 575: 573: 563: 554: 545: 543: 533: 524: 522: 512: 503: 499: 491: 486: 483: 481: 478: 476: 473: 472: 471: 470: 458: 455: 450: 447: 444: 440: 439: 437: 434:** 1 × 20-mm 433: 430: 429: 428: 425: 417: 414: 411: 408: 405: 402: 399: 398:Cruise speed: 396: 393: 390: 389: 388: 386: 378: 374: 371: 368: 364: 360: 357: 354: 353:Gross weight: 351: 348: 347:Empty weight: 345: 342: 339: 336: 333: 330: 327: 324: 321: 318: 315: 314: 313: 311: 306: 304: 292: 288: 285: 282: 279: 276: 273: 270: 267: 264: 261: 260: 254: 252: 247: 245: 241: 236: 235: 230: 226: 222: 216: 214: 210: 206: 203: 199: 195: 191: 187: 183: 179: 175: 171: 167: 162: 160: 156: 152: 148: 144: 140: 136: 132: 122: 120: 117:bombers, the 116: 112: 108: 104: 100: 96: 92: 88: 78: 73: 72: 68: 66:First flight 65: 64: 61: 58: 56:Manufacturer 55: 54: 51: 48: 43: 42: 35: 32: 31: 27: 22: 17: 894:Chardonneret 707: 651:SNCAC NC.150 637: 623: 606: 598: 589: 562: 553: 532: 511: 502: 490: 468: 467: 456: 431: 423: 421: 415: 409: 403: 397: 391: 384: 382: 372: 358: 352: 346: 340: 334: 328: 322: 316: 309: 307: 302: 301: 248: 239: 232: 217: 209:supercharger 169: 165: 163: 130: 128: 107:supercharger 87:SNCAC NC.150 86: 84: 75:Number built 69:11 May 1939 653:. (Russian) 385:Performance 373:Powerplant: 367:V12 engines 359:Powerplant: 205:V12 engines 147:pressurised 919:Categories 617:References 607:Aviafrance 341:Wing area: 159:Air France 889:Belphégor 696:by number 480:Amiot 354 329:Wingspan: 303:Data from 274:NC.151.03 268:NC.150.02 262:NC.150.01 229:Amiot 354 198:twin tail 188:, wooden 174:monoplane 151:mailplane 115:Amiot 354 103:monoplane 904:Martinet 899:Cormoran 464:See also 446:MAC 1934 424:Armament 257:Variants 884:Abeille 877:by name 868:NC.3021 853:NC.2001 848:NC 1080 843:NC.1071 838:NC.1070 748:NC.47-2 743:NC.47-1 738:NC.47-0 723:NC.4-10 335:Height: 323:Length: 194:plywood 143:Hanriot 19:NC.150 863:NC.271 858:NC 211 833:NC.900 828:NC.860 823:NC.856 818:NC.855 813:NC.854 808:NC.853 803:NC.851 798:NC.850 793:NC.841 788:NC.840 783:NC.832 778:NC.702 773:NC.701 768:NC.700 763:NC.600 758:NC.530 753:NC.510 733:NC.433 728:NC.420 718:NC.223 713:NC.211 708:NC.150 703:NC.130 630:  457:Bombs: 443:7.5 mm 404:Range: 286:NC.153 280:NC.152 240:bi-tri 170:NC.150 166:NC.140 91:French 50:France 494:Notes 432:Guns: 317:Crew: 186:spars 135:SNCAC 60:SNCAC 33:Role 628:ISBN 441:1 × 375:1 × 361:2 × 319:Four 227:and 192:and 190:ribs 141:and 113:and 85:The 921:: 605:. 571:^ 541:^ 520:^ 246:. 161:. 79:1 680:e 673:t 666:v 238:" 133:(

Index


France
SNCAC
French
bomber aircraft
Second World War
monoplane
supercharger
Lioré et Olivier LeO 45
Amiot 354
surrender of France
SNCAC
Farman Aviation Works
Hanriot
pressurised
mailplane
Farman F.223.3
Air France
monoplane
tailwheel undercarriage
strategic materials
spars
ribs
plywood
twin tail
Hispano-Suiza 12Y
V12 engines
supercharger
Hispano-Suiza 12X
Toussus-le-Noble

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