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Turbomeca Bastan

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engine developed in France in 1957. Early models developed 650 shp (485 kW), but by 1965 this had been increased to 1,048 shp (780 kW) with the
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flying test bed. The engine's principal applications were the
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Flight tests of some Bastan models were carried out using a
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helicopters. De-rated to 1,119 kW (1,500 hp)
252:A paired Bastan IV developed for French-modified 807: 501:. Wellingborough: Patrick Stephens. p. 164. 447: 445: 443: 441: 482: 260: 533: 469: 467: 465: 463: 434:. London: Sampson, Low, Marston & Co Ltd. 438: 296:685 mm (26.97 in) width, 775.5 mm (30.53 in) 425: 423: 547: 540: 526: 460: 273: 473: 451: 430:Taylor, John W.R. FRHistS. ARAeS (1962). 269:Janes's All The World's Aircraft 1965-66. 420: 152: 44:showing the Bastan engines as installed 511:Jane's All The World's Aircraft 1965-66 496: 432:Jane's All the World's Aircraft 1962-63 146:The Bastan was also developed into the 808: 505: 429: 16:1950s French turboprop aircraft engine 521: 454:Aircraft engines of the World 1964-65 157:A Bastan under test, mounted above a 42:Dinard–Pleurtuit–Saint-Malo Airport 13: 499:World Encyclopedia of Aero Engines 476:Aircraft engines of the World 1970 14: 832: 27: 165: 513:. London: Samson Low, Marston. 344: 1: 413: 306: 192:Sud Aviation SE.117 Voltigeur 187:Sud Aviation SE.116 Voltigeur 371:352 g/kWh (0.578 lb/eshp hr) 7: 474:Wilkinson, Paul H. (1970). 452:Wilkinson, Paul H. (1964). 384: 261:Specifications (Bastan VIC) 197: 10: 837: 816:Turbomeca aircraft engines 779: 753: 735:MTU Turbomeca Rolls-Royce 733: 726: 653: 625: 582: 558: 488:Taylor 1965, pp. 461–462. 367:Specific fuel consumption 319:followed by single-stage 35: 26: 21: 408:List of aircraft engines 331:Direct flow annular type 821:1950s turboprop engines 274:General characteristics 497:Gunston, Bill (1986). 380:3.7 kW/kg (2.3 lb/ehp) 358:Overall pressure ratio 340:Three-stage axial flow 321:centrifugal compressor 162: 159:Lockheed Constellation 133:Lockheed Constellation 755:Rolls-Royce Turbomeca 561:Auxiliary power units 376:Power-to-weight ratio 351:Maximum power output: 156: 177:FMA IA 50 GuaranĂ­ II 390:Related development 507:Taylor, John W. R. 396:Turbomeca Aubisque 353:794 kW (1,065 ehp) 290:2,034 mm (80.1 in) 172:AĂ©rospatiale N 262 163: 148:Turbomeca Aubisque 137:AĂ©rospatiale N 262 109:Turbomeca Aubisque 93:AĂ©rospatiale N 262 88:Major applications 803: 802: 799: 798: 727:Joint development 114: 113: 828: 731: 730: 542: 535: 528: 519: 518: 514: 502: 489: 486: 480: 479: 471: 458: 457: 449: 436: 435: 427: 317:axial compressor 118:Turbomeca Bastan 105: 89: 61: 31: 19: 18: 836: 835: 831: 830: 829: 827: 826: 825: 806: 805: 804: 795: 775: 749: 722: 649: 621: 578: 559:Gas generators/ 554: 546: 493: 492: 487: 483: 472: 461: 450: 439: 428: 421: 416: 387: 347: 309: 302:212 kg (467 lb) 276: 263: 200: 168: 139:(Nord 262) and 103: 95: 87: 60:National origin 59: 17: 12: 11: 5: 834: 824: 823: 818: 801: 800: 797: 796: 794: 793: 786: 784: 777: 776: 774: 773: 767: 760: 758: 751: 750: 748: 747: 740: 738: 728: 724: 723: 721: 720: 715: 710: 705: 700: 695: 689: 684: 679: 674: 669: 663: 661: 651: 650: 648: 647: 642: 637: 631: 629: 623: 622: 620: 619: 614: 609: 604: 599: 594: 588: 586: 580: 579: 577: 576: 571: 565: 563: 556: 555: 545: 544: 537: 530: 522: 516: 515: 503: 491: 490: 481: 459: 437: 418: 417: 415: 412: 411: 410: 399: 398: 386: 383: 382: 381: 372: 363: 354: 346: 343: 342: 341: 332: 323: 308: 305: 304: 303: 297: 291: 285: 275: 272: 262: 259: 258: 257: 250: 247: 245: 242: 240: 237: 235: 232: 230: 227: 225: 222: 220: 217: 214: 211: 209: 206: 204: 199: 196: 195: 194: 189: 184: 179: 174: 167: 164: 112: 111: 106: 104:Developed into 100: 99: 90: 84: 83: 80: 76: 75: 70: 66: 65: 62: 56: 55: 50: 46: 45: 33: 32: 24: 23: 15: 9: 6: 4: 3: 2: 833: 822: 819: 817: 814: 813: 811: 791: 788: 787: 785: 782: 778: 771: 768: 765: 762: 761: 759: 756: 752: 745: 742: 741: 739: 736: 732: 729: 725: 719: 716: 714: 711: 709: 706: 704: 701: 699: 696: 693: 690: 688: 685: 683: 680: 678: 675: 673: 670: 668: 665: 664: 662: 660: 656: 652: 646: 643: 641: 638: 636: 633: 632: 630: 628: 624: 618: 615: 613: 610: 608: 605: 603: 600: 598: 595: 593: 590: 589: 587: 585: 581: 575: 572: 570: 567: 566: 564: 562: 557: 553: 550: 543: 538: 536: 531: 529: 524: 523: 520: 512: 508: 504: 500: 495: 494: 485: 477: 470: 468: 466: 464: 455: 448: 446: 444: 442: 433: 426: 424: 419: 409: 406: 405: 404: 403: 402:Related lists 397: 394: 393: 392: 391: 379: 377: 373: 370: 368: 364: 361: 359: 355: 352: 349: 348: 339: 337: 333: 330: 328: 324: 322: 318: 315:Single-stage 314: 311: 310: 301: 298: 295: 292: 289: 286: 284: 281: 278: 277: 271: 270: 267: 255: 254:Sikorsky S-58 251: 248: 246: 243: 241: 238: 236: 233: 231: 228: 226: 223: 221: 218: 215: 212: 210: 207: 205: 202: 201: 193: 190: 188: 185: 183: 180: 178: 175: 173: 170: 169: 160: 155: 151: 149: 144: 142: 138: 134: 129: 127: 123: 119: 110: 107: 102: 101: 98: 94: 91: 86: 85: 81: 78: 77: 74: 71: 69:Manufacturer 68: 67: 63: 58: 57: 54: 51: 48: 47: 43: 39: 34: 30: 25: 20: 772:(Turboshaft) 746:(Turboshaft) 702: 552:aero engines 510: 498: 484: 475: 453: 431: 401: 400: 389: 388: 374: 365: 356: 350: 334: 325: 312: 299: 293: 287: 279: 268: 265: 264: 249:Bi-Bastan IV 166:Applications 145: 130: 125: 117: 115: 783:/Turbomeca: 659:Turboshafts 345:Performance 313:Compressor: 300:Dry weight: 229:Bastan VIC1 219:Bastan VIB2 216:Bastan VIB1 213:Bastan VIA1 143:airliners. 810:Categories 792:(Turbofan) 766:(Turbofan) 655:Turboprops 414:References 327:Combustors 307:Components 234:Bastan VII 224:Bastan VIC 150:turbofan. 126:Bastan VII 79:First run 694:/Marcadau 627:Turbofans 584:Turbojets 549:Turbomeca 294:Diameter: 283:Turboprop 266:Data from 239:Bastan 16 208:Bastan VI 203:Bastan IV 122:turboprop 73:Turbomeca 53:Turboprop 692:Artouste 645:Aubisque 574:Palouste 509:(1965). 385:See also 244:Bastafan 198:Variants 182:Nord 260 141:Nord 260 97:Nord 260 38:Nord 262 698:Astazou 672:Ardiden 640:Astafan 602:MarborĂ© 592:Arbizon 336:Turbine 288:Length: 161:in 1977 64:France 22:Bastan 790:Larzac 781:Snecma 770:RTM322 744:MTR390 713:TM 333 708:Makila 703:Bastan 687:Arrius 682:Arriel 677:Arrano 617:PimĂ©nĂ© 597:Gabizo 569:OrĂ©don 362:5.83:1 120:was a 764:Adour 718:Turmo 667:Aneto 635:Aspin 612:Palas 607:Ossau 280:Type: 82:1957 49:Type 116:The 40:at 812:: 462:^ 440:^ 422:^ 128:. 36:A 757:: 737:: 657:/ 541:e 534:t 527:v 378:: 369:: 360:: 338:: 329::

Index


Nord 262
Dinard–Pleurtuit–Saint-Malo Airport
Turboprop
Turbomeca
AĂ©rospatiale N 262
Nord 260
Turbomeca Aubisque
turboprop
Lockheed Constellation
AĂ©rospatiale N 262
Nord 260
Turbomeca Aubisque

Lockheed Constellation
AĂ©rospatiale N 262
FMA IA 50 GuaranĂ­ II
Nord 260
Sud Aviation SE.116 Voltigeur
Sud Aviation SE.117 Voltigeur
Sikorsky S-58
Turboprop
axial compressor
centrifugal compressor
Combustors
Turbine
Overall pressure ratio
Specific fuel consumption
Power-to-weight ratio
Turbomeca Aubisque

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