Knowledge (XXG)

KDU-414

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thermal protection cowl containing the spherical propellant tank. A barrier splits the tank into two separate compartments, filled with the propellant,
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Osnovy teorii i rascheta zhidkostnykh raketnykh dvigateley Kn. 2 - Fundamentals of the theory and calculation of liquid rocket engines - Book 2
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The Corrective Propulsion Unit consists of a single chamber 'S5.19' liquid rocket engine and a
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In 1974, it was replaced with its derived successor, the KDU-414A with the S5.114 engine.
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KDU-414 as seen on the "Russia in Space" exhibition (Airport Frankfurt, Germany, 2002)
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Russian Planetary Exploration: History, Development, Legacy and Prospects
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The Superpower Space Race: An Explosive Rivalry through the Solar System
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Soviet Robots in the Solar System: Mission Technologies and Discoveries
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Kosmonavtika Entsiklopediya - Cosmonautic Encyclopedia
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T. Huntress, JR., Wesley; Ya Marov, Mikhail (2011).
928: 891: 713: 357:, respectively. This combination of propellants is 253: 245: 237: 229: 224: 216: 208: 200: 189: 178: 168: 158: 153: 145: 140: 130: 122: 108: 101: 93: 82: 72: 62: 54: 46: 36: 398: 396: 394: 392: 302:Propulsion Unit developed and produced by the 693: 613: 611: 609: 293:Russian Корректирующая Двигательная Установка 8: 376:allows the engine to swivel along two axes. 19: 997:Rocket engines using the pressure-fed cycle 992:Rocket engines using hypergolic propellant 700: 686: 678: 560:: CS1 maint: location missing publisher ( 467:. Moscow: Vysshaya Shkola. p. 20-21. 409:. Springer Verlag, Praxis Publishing Ltd. 25: 486: 484: 388: 553: 18: 295:, Corrective Propulsion Unit), is a 7: 641:"Inventing The Interplanetary Probe" 629:from the original on 18 March 2022. 987:Rocket engines of the Soviet Union 651:from the original on 8 April 2022. 550:from the original on 11 July 2022. 449:from the original on 23 July 2021. 14: 260:Molniya satellites (First series) 882: 665: 511:from the original on 2022-07-10. 497:. Springer Verlag. p. 195. 595:from the original on 2022-07-10 423:from the original on 2022-07-10 365:, which doubles as a source of 1: 708:Spacecraft engines and motors 460:V. M., Kudryavtseva (1993). 314:as well as the space probes 89:& Mid-course corrections 1002:Spacecraft attitude control 1018: 977:KB KhimMash rocket engines 880: 537:Космонавтика Энциклопедия 258: 24: 536: 531:Gluschko, V. P. (1985). 464: 892:Solid propellant motors 543:. Moscow. p. 159. 491:Reeves, Robert (2007). 403:Harvey, Brian (2007). 170:Thrust-to-weight ratio 936:Spacecraft propulsion 16:Type of rocket engine 956:Liquid apogee engine 674:at Wikimedia Commons 353:, and the oxidizer, 304:Isayev Design Bureau 185:1.18 MPa / 11.80 bar 77:Isayev Design Bureau 645:mentallandscape.com 217:Propellant capacity 162:445.5 lbf / 202 kgf 21: 308:Molniya satellites 103:Liquid-fuel engine 964: 963: 951:Apogee kick motor 670:Media related to 441:Brügge, Norbert. 312:Kosmos satellites 285: 284: 264:Kosmos satellites 37:Country of origin 1009: 929:Related articles 886: 885: 702: 695: 688: 679: 669: 653: 652: 637: 631: 630: 615: 604: 603: 601: 600: 572: 566: 565: 559: 551: 549: 542: 528: 513: 512: 488: 479: 478: 457: 451: 450: 438: 432: 431: 429: 428: 400: 363:gaseous nitrogen 241:2.42 ft / 0.74 m 233:3.34 ft / 1.02 m 191:Specific impulse 87:Attitude Control 29: 22: 1017: 1016: 1012: 1011: 1010: 1008: 1007: 1006: 967: 966: 965: 960: 924: 887: 883: 878: 709: 706: 662: 657: 656: 639: 638: 634: 623:astronautix.com 617: 616: 607: 598: 596: 589: 574: 573: 569: 552: 547: 540: 538: 530: 529: 516: 505: 490: 489: 482: 475: 466: 459: 458: 454: 440: 439: 435: 426: 424: 417: 402: 401: 390: 385: 278: 274: 270: 266: 262: 163: 32: 17: 12: 11: 5: 1015: 1013: 1005: 1004: 999: 994: 989: 984: 982:Rocket engines 979: 969: 968: 962: 961: 959: 958: 953: 948: 943: 938: 932: 930: 926: 925: 923: 922: 919: 916: 911: 906: 901: 895: 893: 889: 888: 881: 879: 877: 876: 871: 866: 861: 856: 851: 846: 841: 840: 839: 831: 826: 821: 816: 811: 806: 805: 804: 799: 794: 791: 786: 778: 777: 776: 773: 770: 767: 759: 758: 757: 754: 746: 741: 736: 731: 726: 720: 718: 711: 710: 707: 705: 704: 697: 690: 682: 676: 675: 661: 660:External links 658: 655: 654: 632: 605: 588:978-1441978974 587: 567: 514: 504:978-0306447686 503: 480: 473: 452: 433: 416:978-0387463438 415: 387: 386: 384: 381: 367:RCS propellant 283: 282: 256: 255: 251: 250: 249:134 lb / 61 kg 247: 243: 242: 239: 235: 234: 231: 227: 226: 222: 221: 218: 214: 213: 210: 206: 205: 202: 198: 197: 194: 187: 186: 183: 176: 175: 172: 166: 165: 160: 159:Thrust, vacuum 156: 155: 151: 150: 149:Single chamber 147: 143: 142: 138: 137: 132: 128: 127: 124: 120: 119: 110: 106: 105: 99: 98: 95: 91: 90: 84: 80: 79: 74: 70: 69: 64: 60: 59: 56: 52: 51: 48: 44: 43: 38: 34: 33: 30: 15: 13: 10: 9: 6: 4: 3: 2: 1014: 1003: 1000: 998: 995: 993: 990: 988: 985: 983: 980: 978: 975: 974: 972: 957: 954: 952: 949: 947: 944: 942: 939: 937: 934: 933: 931: 927: 920: 917: 915: 912: 910: 907: 905: 902: 900: 897: 896: 894: 890: 875: 872: 870: 867: 865: 862: 860: 857: 855: 852: 850: 847: 845: 842: 837: 836: 835: 832: 830: 827: 825: 822: 820: 817: 815: 812: 810: 807: 803: 800: 798: 795: 792: 790: 787: 784: 783: 782: 779: 774: 771: 768: 765: 764: 763: 760: 755: 752: 751: 750: 747: 745: 742: 740: 737: 735: 732: 730: 727: 725: 722: 721: 719: 716: 712: 703: 698: 696: 691: 689: 684: 683: 680: 673: 668: 664: 663: 659: 650: 646: 642: 636: 633: 628: 624: 620: 614: 612: 610: 606: 594: 590: 584: 580: 579: 571: 568: 563: 557: 546: 539: 535: 527: 525: 523: 521: 519: 515: 510: 506: 500: 496: 495: 487: 485: 481: 476: 470: 463: 456: 453: 448: 444: 437: 434: 422: 418: 412: 408: 407: 399: 397: 395: 393: 389: 382: 380: 377: 375: 370: 368: 364: 360: 356: 352: 348: 343: 341: 337: 333: 329: 325: 321: 317: 313: 309: 305: 301: 300:liquid rocket 298: 294: 290: 281: 277: 273: 269: 265: 261: 257: 252: 248: 244: 240: 236: 232: 228: 223: 220:77 lb / 35 kg 219: 215: 211: 207: 203: 199: 195: 192: 188: 184: 182: 177: 173: 171: 167: 161: 157: 152: 148: 144: 141:Configuration 139: 136: 133: 129: 125: 123:Mixture ratio 121: 118: 114: 111: 107: 104: 100: 96: 92: 88: 85: 81: 78: 75: 71: 68: 67:Aleksei Isaev 65: 61: 57: 53: 49: 45: 42: 39: 35: 28: 23: 748: 644: 635: 622: 597:. 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Retrieved 405: 378: 374:gimbal mount 371: 344: 297:pressure-fed 292: 288: 286: 135:Pressure-fed 73:Manufacturer 47:First flight 41:Soviet Union 715:Liquid fuel 154:Performance 83:Application 55:Last flight 971:Categories 941:Spacecraft 864:SuperDraco 599:2022-07-10 474:5060025632 427:2022-07-10 383:References 359:hypergolic 310:, several 225:Dimensions 109:Propellant 946:Satellite 921:SpaB-140C 619:"KDU-414" 556:cite book 201:Burn time 94:Successor 809:KTDU-425 649:Archived 627:Archived 593:Archived 545:Archived 509:Archived 447:Archived 421:Archived 320:Venera 1 272:Venera 1 246:Dry mass 238:Diameter 209:Restarts 193:, vacuum 181:pressure 179:Chamber 97:KDU-414A 63:Designer 918:SpaB-65 904:Star 48 899:Star 37 781:KTDU-80 762:KTDU-35 749:KDU-414 717:engines 672:KDU-414 347:conical 289:KDU-414 254:Used in 164:1.96 kN 146:Chamber 20:KDU-414 869:TR-201 802:S5.142 789:11D428 785:11D426 756:S5.114 585:  501:  471:  413:  332:KAUR-2 328:Zond 3 324:Zond 2 316:Mars 1 280:Zond 3 276:Zond 2 268:Mars 1 230:Length 914:FG-36 909:FG-15 874:XLR81 859:S5.92 844:RS-25 838:11D58 834:RD-58 814:LEROS 797:S5.80 793:S5.79 775:S5-66 772:S5-60 769:S5.53 766:S5-35 753:S5.19 744:Draco 739:Curie 724:17D61 548:(PDF) 541:(PDF) 355:IRFNA 196:272 s 131:Cycle 113:IRFNA 854:S5.4 849:S400 829:R-4D 824:LMDE 819:LMAE 734:BT-4 729:AJ10 583:ISBN 562:link 499:ISBN 469:ISBN 411:ISBN 351:UDMH 338:and 326:and 287:The 204:40 s 174:3.27 117:UDMH 58:1974 50:1960 340:3MV 336:2MV 126:2.6 973:: 647:. 643:. 625:. 621:. 608:^ 591:. 558:}} 554:{{ 517:^ 507:. 483:^ 445:. 419:. 391:^ 372:A 342:. 334:, 322:, 318:, 115:/ 701:e 694:t 687:v 602:. 564:) 477:. 430:. 291:( 212:2

Index


Soviet Union
Aleksei Isaev
Isayev Design Bureau
Attitude Control
Liquid-fuel engine
IRFNA
UDMH
Pressure-fed
Thrust-to-weight ratio
pressure
Specific impulse
Molniya satellites (First series)
Kosmos satellites
Mars 1
Venera 1
Zond 2
Zond 3
pressure-fed
liquid rocket
Isayev Design Bureau
Molniya satellites
Kosmos satellites
Mars 1
Venera 1
Zond 2
Zond 3
KAUR-2
2MV
3MV

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