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Nakajima Mamoru

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244:('heavenly mountain') carrier based torpedo bomber aircraft. The Navy requested this aircraft based on the Kasei, but Nakajima's Kenichi Matsumara insisted on using their Mamoru. The B6N first flew on 14 March 1941, demonstrating several problems, notably the poor engine reliability. With the delay of 2 years, by 1943 the engine had improved to the point where serial production was allowed to start, but after only 133 B6N1s had been delivered the Navy ordered the switch to the 1,850 hp (1380 kW) Mitsubishi MK4T Kasei 25. The rest of the 1,268 B6N2s were Kasei powered. 29: 228:
as Japan's first four-engine bomber and proved to be a disappointment. These problems were compounded by the unreliability of the early Mamoru engines, which had to be de-tuned and left the G5N1 underpowered. The G5N1's maiden flight was on 10 April 1941, and a further four prototypes were built with
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engines and redesignated G5N2s. Although the Mitsubishi engines were more reliable than the original Mamoru 11s, further development was halted. Of the six completed Shinzans, four of them (two G5N2s and two G5N1s re-engined with the Kasei 12) were relegated for use as long-range Navy transports
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The Mamoru was Nakajima's seventh air-cooled design, which led to its designation: N for Nakajima, K for air-cooled, 7 for the 7th design, and A for the major model number. Two sub-models were built with minor changes, the Model 11 for the Navy, and the Model 12 for the Army. Both produced
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At some 44.9 litres (2,740 in) displacement, it was one of the largest-displacement 14-cylinder radial engines in the world, rivalling the similar configuration American 42.7 litre (2,600 in)
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engine, the Mamoru proved to be unreliable and was rarely able to operate near its design power. Designs based on the Mamoru were forced to use other engines, typically the less powerful
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engine was a 14-cylinder, air-cooled, two-row radial engine of 1870 hp. The Nakajima model designation for this engine was
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the Mamoru. In an attempt to salvage the project, two additional airframes were fitted with 1,530 hp Mitsubishi MK4B 12
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Francillon, Ph.D., René J. Japanese Aircraft of the Pacific War. London: Putnam & Company, 2nd edition 1979.
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engine of displacement levels, and was meant to compete with early 18-cyl engines, like the 53.6 L
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by the Army and "Mamori" or "Mamoru" by the Navy. According to unified designation code it was
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1,600 horsepower (1,200 kW), 2,500 rpm at 4,900 metres (16,100 ft)
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1,750 horsepower (1,300 kW), 2,500 rpm at 1,400 metres (4,600 ft)
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takeoff: 1,870 hp at 2,600 rpm, cruise: 1,750 hp at 2,500 rpm at 1,400 m
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The first application of the Mamoru was on the first prototype of the
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while it was an experimental project, in service it was known as the
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Pushrod operated overhead-valve system with 4 valves per cylinder
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14-cylinder supercharged, air-cooled two-row radial piston engine
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under the designation Shinzan-Kai Model 12 Transport G5N2-L.
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4 X 1,870 hp (1395 kW) Nakajima NK7A Mamoru 11
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1,870 horsepower (1,390 kW) at 2,600 rpm (take-off)
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1 X 1,870 hp (1395 kW) Nakajima NK7A Mamoru 11
178:, translates as 'to guard, protect, defend and obey'. 302:Specifications (Nakajima NK7A Mamoru type 11, 12) 224:. The G5N1 had been designed on the basis of the 846: 519: 147: 141: 650: 573: 559: 520:Goodwin, Mike & Starkings, Peter (2017). 297:(prototype) 2 X 1,870 hp Nakajima Ha-103 185:engine, of Soviet 41.2 litre (2,515 in) 657: 643: 566: 552: 314: 865:Aircraft air-cooled radial piston engines 237:The Nakajima Mamoru was also used on the 211: 847: 638: 547: 487: 16:1940s Japanese piston aircraft engine 13: 666:Imperial Japanese Army Air Service 390:Two-speed single stage centrifugal 14: 876: 539: 291:2 X 1,870 hp Nakajima Ha-103 196:Competing against the successful 524:. Sandomierz, Poland: MMPBooks. 27: 522:Japanese Aero-Engines 1910-1945 502: 270: 174:translates as 'protection' and 409: 36:Nakajima Mamoru engine at the 1: 860:1940s aircraft piston engines 475: 369: 38:National Air and Space Museum 365:870-903 kg (1,918-1,991 lb.) 7: 431: 247: 148: 10: 881: 453:Pratt & Whitney R-2800 183:Wright R-2600 Twin Cyclone 855:Nakajima aircraft engines 806: 755: 734: 673: 584: 142: 61:Nakajima Aircraft Company 35: 26: 21: 668:aero engine designations 494:translated at eudict.com 480: 470:List of aircraft engines 315:General characteristics 126:Ha-107, Ha-117, Ha-217 212:Design and development 350:44.9 L (2,740 cu in) 222:Nakajima G5N1 Genzan 356:1,380 mm (54.3 in.) 162:, and known as the 437:Comparable engines 84:Major applications 842: 841: 632: 631: 531:978-83-65281-32-6 423:Compression ratio 310:Francillon p. 433 191:Bristol Centaurus 130: 129: 872: 659: 652: 645: 636: 635: 578:aircraft engines 568: 561: 554: 545: 544: 535: 496: 491: 448:Mitsubishi Kasei 341:170 mm (6.7 in.) 332:155 mm (6.1 in.) 295:Mitsubishi Ki-67 263:Mamoru 12 Ha-103 202:Mitsubishi Kasei 198:Mitsubishi Kasei 153: 151: 145: 144: 123: 111: 101: 85: 31: 19: 18: 880: 879: 875: 874: 873: 871: 870: 869: 845: 844: 843: 838: 802: 751: 730: 669: 663: 633: 628: 580: 572: 542: 532: 505: 500: 499: 492: 488: 483: 478: 434: 412: 394:Cooling system: 372: 317: 304: 273: 259: 257: 250: 214: 206:Nakajima Homare 187:Shvetsov ASh-82 139: 121: 115:Nakajima Hikari 109: 99: 83: 70:Kiyoshi Tanaka 51:aircraft engine 17: 12: 11: 5: 878: 868: 867: 862: 857: 840: 839: 837: 836: 831: 826: 821: 816: 810: 808: 804: 803: 801: 800: 795: 790: 785: 780: 775: 770: 765: 759: 757: 753: 752: 750: 749: 744: 738: 736: 732: 731: 729: 728: 723: 718: 713: 708: 703: 698: 693: 688: 683: 677: 675: 671: 670: 662: 661: 654: 647: 639: 630: 629: 627: 626: 621: 616: 611: 606: 601: 596: 590: 588: 586:Piston engines 582: 581: 571: 570: 563: 556: 548: 541: 540:External links 538: 537: 536: 530: 517: 504: 501: 498: 497: 485: 484: 482: 479: 477: 474: 473: 472: 461: 460: 455: 450: 445: 433: 430: 429: 428: 419: 411: 408: 407: 406: 401:Reduction gear 397: 391: 382: 371: 368: 367: 366: 357: 351: 342: 333: 324: 316: 313: 303: 300: 299: 298: 292: 289:Nakajima Ki-49 286: 280: 272: 269: 268: 267: 264: 261: 254: 253:Mamoru 11 NK7A 249: 246: 217:1,850 hp 213: 210: 128: 127: 124: 122:Developed into 118: 117: 112: 110:Developed from 106: 105: 102: 96: 95: 86: 80: 79: 76: 72: 71: 68: 64: 63: 58: 54: 53: 45: 41: 40: 33: 32: 24: 23: 15: 9: 6: 4: 3: 2: 877: 866: 863: 861: 858: 856: 853: 852: 850: 835: 832: 830: 827: 825: 822: 820: 817: 815: 812: 811: 809: 805: 799: 796: 794: 791: 789: 786: 784: 781: 779: 776: 774: 771: 769: 766: 764: 761: 760: 758: 754: 748: 745: 743: 740: 739: 737: 733: 727: 724: 722: 719: 717: 714: 712: 709: 707: 704: 702: 699: 697: 694: 692: 689: 687: 684: 682: 679: 678: 676: 672: 667: 660: 655: 653: 648: 646: 641: 640: 637: 625: 622: 620: 617: 615: 612: 610: 609:Ha-103 Mamoru 607: 605: 602: 600: 597: 595: 594:Ha-1 Kotobuki 592: 591: 589: 587: 583: 579: 576: 569: 564: 562: 557: 555: 550: 549: 546: 533: 527: 523: 518: 515: 514:0-370-30251-6 511: 507: 506: 495: 490: 486: 471: 468: 467: 466: 465: 464:Related lists 459: 458:Wright R-2600 456: 454: 451: 449: 446: 444: 441: 440: 439: 438: 426: 424: 420: 417: 416:Power output: 414: 413: 404: 402: 398: 395: 392: 389: 387: 383: 380: 378: 374: 373: 364: 362: 358: 355: 352: 349: 347: 343: 340: 338: 334: 331: 329: 325: 322: 319: 318: 312: 311: 308: 296: 293: 290: 287: 284: 281: 278: 275: 274: 265: 262: 255: 252: 251: 245: 243: 240: 235: 232: 227: 226:Douglas DC-4E 223: 218: 209: 207: 203: 199: 194: 192: 188: 184: 179: 177: 173: 169: 165: 161: 157: 150: 138: 137: 125: 120: 119: 116: 113: 108: 107: 103: 98: 97: 94: 90: 87: 82: 81: 77: 74: 73: 69: 66: 65: 62: 59: 57:Manufacturer 56: 55: 52: 49: 46: 43: 42: 39: 34: 30: 25: 20: 772: 619:Ha-45 Homare 608: 521: 503:Bibliography 489: 463: 462: 436: 435: 421: 415: 399: 393: 386:Supercharger 384: 375: 359: 353: 346:Displacement 344: 335: 326: 320: 309: 306: 305: 283:Nakajima G5N 277:Nakajima B6N 271:Applications 241: 239:Nakajima B6N 236: 230: 219: 215: 195: 180: 175: 171: 167: 163: 159: 155: 135: 133: 131: 100:Number built 93:Nakajima B6N 89:Nakajima G5N 604:Ha-8 Hikari 410:Performance 849:Categories 476:References 396:Air-cooled 377:Valvetrain 370:Components 361:Dry weight 75:First run 354:Diameter: 307:Data from 134:Nakajima 67:Designer 575:Nakajima 516:. pg 425 432:See also 248:Variants 149:Preserve 756:101-200 443:BMW 801 266:As NK7A 204:or the 22:Mamoru 834:Ha-505 829:Ha-217 824:Ha-214 819:Ha-211 814:Ha-201 798:Ha-140 793:Ha-115 788:Ha-112 783:Ha-105 778:Ha-104 773:Ha-103 768:Ha-102 763:Ha-101 735:51-100 624:Ha-219 528:  512:  337:Stroke 242:Tenzan 176:Mamoru 172:Mamori 164:Ha-103 136:Mamoru 48:Piston 747:Ha-70 742:Ha-60 726:Ha-45 721:Ha-44 716:Ha-40 711:Ha-35 706:Ha-26 701:Ha-25 614:Sakae 481:Notes 405:0.578 321:Type: 231:Kasei 168:Ha-36 78:1941 44:Type 807:200- 696:Ha-9 691:Ha-6 686:Ha-5 681:Ha-1 674:1-50 599:Ha-5 526:ISBN 510:ISBN 328:Bore 132:The 104:200 427:6.5 193:. 160:NK7 156:NAK 851:: 146:, 91:, 658:e 651:t 644:v 567:e 560:t 553:v 534:. 425:: 403:: 388:: 379:: 363:: 348:: 339:: 330:: 152:) 143:護 140:(

Index


National Air and Space Museum
Piston
aircraft engine
Nakajima Aircraft Company
Nakajima G5N
Nakajima B6N
Nakajima Hikari
Wright R-2600 Twin Cyclone
Shvetsov ASh-82
Bristol Centaurus
Mitsubishi Kasei
Mitsubishi Kasei
Nakajima Homare
Nakajima G5N1 Genzan
Douglas DC-4E
Nakajima B6N
Nakajima B6N
Nakajima G5N
Nakajima Ki-49
Mitsubishi Ki-67
Bore
Stroke
Displacement
Dry weight
Valvetrain
Supercharger
Reduction gear
Compression ratio
BMW 801

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