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MMR06

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25: 302: 60:, is a useful starting point for translations, but translators must revise errors as necessary and confirm that the translation is accurate, rather than simply copy-pasting machine-translated text into the English Knowledge. 70: 733: 80:
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738: 151:. The maximum flight height was about 60 - 80 kilometres. Between 1988 and 1992 62 rockets of the type MMR06-M were launched from the former 143:
experiments, with a length of 3.48 metres and a total weight of 130 kg. The MMR06 rocket was built in two versions: One version had a
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Content in this edit is translated from the existing Russian Knowledge article at ]; see its history for attribution.
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top, the second one, named MMR06-M, had a detachable free flying top, also called
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to the source of your translation. A model attribution edit summary is
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to this template: there are already 932 articles in the
53: 725: 95:accompanying your translation by providing an 44:Click for important translation instructions. 36:expand this article with text translated from 734:Meteorological instrumentation and equipment 166: 314: 568: 288:Equatorial moment of inertia at burn-out 307:schematic flight path of MMR06-M rocket 726: 280:Equatorial moment of inertia at launch 739:Sounding rockets of the Soviet Union 18: 614: 267:Axial moment of inertia at burn-out 13: 14: 760: 704: 387: 300: 23: 749:Meteorology in the Soviet Union 639: 431:Length without transition piece 228:center of gravity at burn-out ( 561:Velocity at expulsion of probe 296: 240:Distance from end of nozzle to 226:Distance from end of nozzle to 216:Distance from end of nozzle to 105:You may also add the template 1: 698: 551:Angle of attack between wings 535:Equatorial moment of inertia 423:Length with transition piece 298: 7: 618: 479: 391: 318: 218:center of gravity at launch 175: 77:will aid in categorization. 10: 765: 744:Sounding rockets of Russia 519:to center of wind pressure 52:Machine translation, like 569:Aerodynamic coefficients 517:Distance from end of dart 507:Distance from end of dart 274: 249: 210: 167:Technical data of MMR06-M 38:the corresponding article 415:without transition piece 315:Aerodynamic coefficients 171: 107:{{Translated|ru|ММР-06}} 676: 644: 527:Axial moment of inertia 475: 242:center of wind pressure 116:For more guidance, see 375:rocket around own axis 373:Rotational velocity of 16:Soviet sounding rocket 688:Molodyozhnaya Station 553:and longitudinal axis 405:with transition piece 118:Knowledge:Translation 89:copyright attribution 509:to center of gravity 413:Mass without payload 403:Mass without payload 135:is a Soviet/Russian 711:www.astronautix.com 530:0.00752 kg/m 97:interlanguage link 637: 636: 630:Time of expulsion 612: 611: 473: 472: 395:Mass with payload 385: 384: 365:Burn-out velocity 312: 311: 308: 295: 294: 257:moment of inertia 129: 128: 45: 756: 720: 718: 717: 619: 615:Parachute system 480: 439:Time of burn-out 392: 344:lift coefficient 328:drag coefficient 319: 306: 304: 297: 291:158.5 kg/m 283:394.5 kg/m 176: 108: 102: 76: 75:|topic= 73:, and specifying 58:Google Translate 43: 27: 26: 19: 764: 763: 759: 758: 757: 755: 754: 753: 724: 723: 715: 713: 701: 679: 647: 642: 617: 605: 592: 579: 552: 538:3.48 kg/m 518: 508: 478: 464:Angle of attack 414: 404: 390: 374: 357: 341: 325: 317: 305: 270:0.25 kg/m 262:0.87 kg/m 241: 227: 217: 182:134 ±5 kg 174: 169: 125: 124: 123: 106: 100: 74: 46: 28: 24: 17: 12: 11: 5: 762: 752: 751: 746: 741: 736: 722: 721: 700: 697: 696: 695: 690: 685: 678: 675: 674: 673: 668: 663: 658: 653: 646: 643: 641: 638: 635: 634: 631: 627: 626: 623: 616: 613: 610: 609: 606: 603: 597: 596: 593: 590: 584: 583: 580: 577: 571: 570: 566: 565: 564:3.65 m/s 562: 558: 557: 554: 548: 547: 544: 540: 539: 536: 532: 531: 528: 524: 523: 520: 514: 513: 510: 504: 503: 500: 496: 495: 492: 488: 487: 484: 477: 474: 471: 470: 467: 460: 459: 456: 452: 451: 448: 444: 443: 440: 436: 435: 432: 428: 427: 424: 420: 419: 416: 410: 409: 406: 400: 399: 398:121.8 kg 396: 389: 386: 383: 382: 376: 370: 369: 368:1428 m/s 366: 362: 361: 358: 355: 351: 350: 347: 339: 335: 334: 331: 323: 316: 313: 310: 309: 293: 292: 289: 285: 284: 281: 277: 276: 272: 271: 268: 264: 263: 260: 252: 251: 247: 246: 243: 237: 236: 233: 223: 222: 219: 213: 212: 208: 207: 204: 200: 199: 196: 192: 191: 188: 184: 183: 180: 173: 170: 168: 165: 155:exercise area 141:meteorological 127: 126: 122: 121: 114: 103: 81: 78: 66:adding a topic 61: 50: 47: 33: 32: 31: 29: 22: 15: 9: 6: 4: 3: 2: 761: 750: 747: 745: 742: 740: 737: 735: 732: 731: 729: 712: 708: 703: 702: 694: 691: 689: 686: 684: 681: 680: 672: 669: 667: 664: 662: 661:Ernst Krenkel 659: 657: 654: 652: 649: 648: 632: 629: 628: 624: 621: 620: 607: 602: 599: 598: 594: 589: 586: 585: 581: 576: 573: 572: 567: 563: 560: 559: 555: 550: 549: 545: 542: 541: 537: 534: 533: 529: 526: 525: 521: 516: 515: 511: 506: 505: 501: 498: 497: 493: 490: 489: 486:12.2 kg 485: 482: 481: 468: 465: 462: 461: 457: 454: 453: 449: 446: 445: 442:7.2 s - 12 s 441: 438: 437: 433: 430: 429: 425: 422: 421: 417: 412: 411: 407: 402: 401: 397: 394: 393: 388:Rocket engine 381: 377: 372: 371: 367: 364: 363: 359: 353: 352: 348: 345: 337: 336: 332: 329: 321: 320: 303: 299: 290: 287: 286: 282: 279: 278: 273: 269: 266: 265: 261: 258: 254: 253: 248: 244: 239: 238: 234: 231: 225: 224: 220: 215: 214: 209: 205: 202: 201: 197: 194: 193: 189: 186: 185: 181: 178: 177: 164: 162: 158: 154: 150: 146: 142: 138: 134: 119: 115: 112: 104: 98: 94: 90: 86: 82: 79: 72: 71:main category 68: 67: 62: 59: 55: 51: 49: 48: 41: 39: 34:You can help 30: 21: 20: 714:. Retrieved 710: 705:Wade, Mark. 683:Kapustin Yar 670: 665: 660: 655: 650: 640:Launch sites 600: 587: 574: 230:Brennschluss 132: 130: 93:edit summary 84: 64: 35: 418:33 kg 408:38 kg 198:78 kg 190:58 kg 728:Categories 716:2024-07-01 699:References 625:1 kg 187:Mass empty 179:Total mass 161:atmosphere 40:in Russian 543:Wing span 469:5' - 40' 455:Wing span 259:at launch 195:Fuel mass 111:talk page 63:Consider 707:"MMR-06" 546:0.148 m 502:0.063 m 499:Diameter 494:1.478 m 466:of wings 447:Diameter 434:2.444 m 426:2.813 m 235:1.872 m 221:1.445 m 87:provide 656:Ushakov 512:0.78 m 275:  250:  211:  206:4.14 m 145:conical 109:to the 91:in the 693:Zingst 666:Priliv 651:Musson 633:130 s 522:0.5 m 491:Length 458:0.6 m 450:0.2 m 255:Axial 203:Length 157:Zingst 137:rocket 671:Volna 608:34.4 582:0.15 360:34.4 333:0.42 172:Total 133:MMR06 54:DeepL 677:Land 645:Ship 622:Mass 483:Mass 476:Dart 378:800 245:1 m 149:dart 139:for 131:The 85:must 83:You 595:20 556:0° 380:rpm 349:20 153:NVA 56:or 42:. 730:: 709:. 163:. 719:. 604:m 601:C 591:l 588:C 578:d 575:C 356:m 354:C 346:) 342:( 340:l 338:C 330:) 326:( 324:d 322:C 232:) 120:. 113:.

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edit summary
interlanguage link
talk page
Knowledge:Translation
rocket
meteorological
conical
dart
NVA
Zingst
atmosphere
Brennschluss
moment of inertia
schematic flight path of MMR06-M rocket
drag coefficient
lift coefficient
rpm
Angle of attack
Kapustin Yar
Molodyozhnaya Station
Zingst
"MMR-06"
Categories
Meteorological instrumentation and equipment

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