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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)
263:A paired Bastan IV developed for French-modified 818: 512:. Wellingborough: Patrick Stephens. p. 164. 458: 456: 454: 452: 493: 271: 544: 480: 478: 476: 474: 445:. London: Sampson, Low, Marston & Co Ltd. 449: 307:685 mm (26.97 in) width, 775.5 mm (30.53 in) 436: 434: 558: 551: 537: 471: 284: 484: 462: 441:Taylor, John W.R. FRHistS. ARAeS (1962). 280:Janes's All The World's Aircraft 1965-66. 431: 163: 55:showing the Bastan engines as installed 522:Jane's All The World's Aircraft 1965-66 507: 443:Jane's All the World's Aircraft 1962-63 157:The Bastan was also developed into the 14: 819: 516: 440: 27:1950s French turboprop aircraft engine 532: 465:Aircraft engines of the World 1964-65 168:A Bastan under test, mounted above a 53:Dinard–Pleurtuit–Saint-Malo Airport 24: 510:World Encyclopedia of Aero Engines 487:Aircraft engines of the World 1970 25: 843: 38: 176: 524:. London: Samson Low, Marston. 355: 13: 1: 424: 317: 203:Sud Aviation SE.117 Voltigeur 198:Sud Aviation SE.116 Voltigeur 382:352 g/kWh (0.578 lb/eshp hr) 7: 485:Wilkinson, Paul H. (1970). 463:Wilkinson, Paul H. (1964). 395: 272:Specifications (Bastan VIC) 208: 10: 848: 827:Turbomeca aircraft engines 790: 764: 746:MTU Turbomeca Rolls-Royce 744: 737: 664: 636: 593: 569: 499:Taylor 1965, pp. 461–462. 378:Specific fuel consumption 330:followed by single-stage 46: 37: 32: 419:List of aircraft engines 342:Direct flow annular type 832:1950s turboprop engines 285:General characteristics 508:Gunston, Bill (1986). 391:3.7 kW/kg (2.3 lb/ehp) 369:Overall pressure ratio 351:Three-stage axial flow 332:centrifugal compressor 173: 170:Lockheed Constellation 144:Lockheed Constellation 766:Rolls-Royce Turbomeca 572:Auxiliary power units 387:Power-to-weight ratio 362:Maximum power output: 167: 188:FMA IA 50 GuaranĂ­ II 401:Related development 18:Turbomeca Bastan IV 518:Taylor, John W. R. 407:Turbomeca Aubisque 364:794 kW (1,065 ehp) 301:2,034 mm (80.1 in) 183:AĂ©rospatiale N 262 174: 159:Turbomeca Aubisque 148:AĂ©rospatiale N 262 120:Turbomeca Aubisque 104:AĂ©rospatiale N 262 99:Major applications 814: 813: 810: 809: 738:Joint development 125: 124: 16:(Redirected from 839: 742: 741: 553: 546: 539: 530: 529: 525: 513: 500: 497: 491: 490: 482: 469: 468: 460: 447: 446: 438: 328:axial compressor 129:Turbomeca Bastan 116: 100: 72: 42: 30: 29: 21: 847: 846: 842: 841: 840: 838: 837: 836: 817: 816: 815: 806: 786: 760: 733: 660: 632: 589: 570:Gas generators/ 565: 557: 504: 503: 498: 494: 483: 472: 461: 450: 439: 432: 427: 398: 358: 320: 313:212 kg (467 lb) 287: 274: 211: 179: 150:(Nord 262) and 114: 106: 98: 71:National origin 70: 28: 23: 22: 15: 12: 11: 5: 845: 835: 834: 829: 812: 811: 808: 807: 805: 804: 797: 795: 788: 787: 785: 784: 778: 771: 769: 762: 761: 759: 758: 751: 749: 739: 735: 734: 732: 731: 726: 721: 716: 711: 706: 700: 695: 690: 685: 680: 674: 672: 662: 661: 659: 658: 653: 648: 642: 640: 634: 633: 631: 630: 625: 620: 615: 610: 605: 599: 597: 591: 590: 588: 587: 582: 576: 574: 567: 566: 556: 555: 548: 541: 533: 527: 526: 514: 502: 501: 492: 470: 448: 429: 428: 426: 423: 422: 421: 410: 409: 397: 394: 393: 392: 383: 374: 365: 357: 354: 353: 352: 343: 334: 319: 316: 315: 314: 308: 302: 296: 286: 283: 273: 270: 269: 268: 261: 258: 256: 253: 251: 248: 246: 243: 241: 238: 236: 233: 231: 228: 225: 222: 220: 217: 215: 210: 207: 206: 205: 200: 195: 190: 185: 178: 175: 123: 122: 117: 115:Developed into 111: 110: 101: 95: 94: 91: 87: 86: 81: 77: 76: 73: 67: 66: 61: 57: 56: 44: 43: 35: 34: 26: 9: 6: 4: 3: 2: 844: 833: 830: 828: 825: 824: 822: 802: 799: 798: 796: 793: 789: 782: 779: 776: 773: 772: 770: 767: 763: 756: 753: 752: 750: 747: 743: 740: 736: 730: 727: 725: 722: 720: 717: 715: 712: 710: 707: 704: 701: 699: 696: 694: 691: 689: 686: 684: 681: 679: 676: 675: 673: 671: 667: 663: 657: 654: 652: 649: 647: 644: 643: 641: 639: 635: 629: 626: 624: 621: 619: 616: 614: 611: 609: 606: 604: 601: 600: 598: 596: 592: 586: 583: 581: 578: 577: 575: 573: 568: 564: 561: 554: 549: 547: 542: 540: 535: 534: 531: 523: 519: 515: 511: 506: 505: 496: 488: 481: 479: 477: 475: 466: 459: 457: 455: 453: 444: 437: 435: 430: 420: 417: 416: 415: 414: 413:Related lists 408: 405: 404: 403: 402: 390: 388: 384: 381: 379: 375: 372: 370: 366: 363: 360: 359: 350: 348: 344: 341: 339: 335: 333: 329: 326:Single-stage 325: 322: 321: 312: 309: 306: 303: 300: 297: 295: 292: 289: 288: 282: 281: 278: 266: 265:Sikorsky S-58 262: 259: 257: 254: 252: 249: 247: 244: 242: 239: 237: 234: 232: 229: 226: 223: 221: 218: 216: 213: 212: 204: 201: 199: 196: 194: 191: 189: 186: 184: 181: 180: 171: 166: 162: 160: 155: 153: 149: 145: 140: 138: 134: 130: 121: 118: 113: 112: 109: 105: 102: 97: 96: 92: 89: 88: 85: 82: 80:Manufacturer 79: 78: 74: 69: 68: 65: 62: 59: 58: 54: 50: 45: 41: 36: 31: 19: 783:(Turboshaft) 757:(Turboshaft) 713: 563:aero engines 521: 509: 495: 486: 464: 442: 412: 411: 400: 399: 385: 376: 367: 361: 345: 336: 323: 310: 304: 298: 290: 279: 276: 275: 260:Bi-Bastan IV 177:Applications 156: 141: 136: 128: 126: 794:/Turbomeca: 670:Turboshafts 356:Performance 324:Compressor: 311:Dry weight: 240:Bastan VIC1 230:Bastan VIB2 227:Bastan VIB1 224:Bastan VIA1 154:airliners. 821:Categories 803:(Turbofan) 777:(Turbofan) 666:Turboprops 425:References 338:Combustors 318:Components 245:Bastan VII 235:Bastan VIC 161:turbofan. 137:Bastan VII 90:First run 705:/Marcadau 638:Turbofans 595:Turbojets 560:Turbomeca 305:Diameter: 294:Turboprop 277:Data from 250:Bastan 16 219:Bastan VI 214:Bastan IV 133:turboprop 84:Turbomeca 64:Turboprop 703:Artouste 656:Aubisque 585:Palouste 520:(1965). 396:See also 255:Bastafan 209:Variants 193:Nord 260 152:Nord 260 108:Nord 260 49:Nord 262 709:Astazou 683:Ardiden 651:Astafan 613:MarborĂ© 603:Arbizon 347:Turbine 299:Length: 172:in 1977 75:France 33:Bastan 801:Larzac 792:Snecma 781:RTM322 755:MTR390 724:TM 333 719:Makila 714:Bastan 698:Arrius 693:Arriel 688:Arrano 628:PimĂ©nĂ© 608:Gabizo 580:OrĂ©don 373:5.83:1 131:was a 775:Adour 729:Turmo 678:Aneto 646:Aspin 623:Palas 618:Ossau 291:Type: 93:1957 60:Type 127:The 51:at 823:: 473:^ 451:^ 433:^ 139:. 47:A 768:: 748:: 668:/ 552:e 545:t 538:v 389:: 380:: 371:: 349:: 340:: 20:)

Index

Turbomeca Bastan IV

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

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