Knowledge (XXG)

Cora (rocket)

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Six Cora launches were planned, the first four using the Cora 1 configuration and the last two using the Cora 2. Only the three first launches took place, with the Cora 2 configuration never being tested:
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The entire rocket had a length of 11.5 metres, a diameter of 2.01 m and a takeoff weight of 16.5 tonnes. Total thrust was 220.00 kN, with the rocket capable of reaching an apogee of 55 km.
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second stage was 3.36 meters long with a diameter of 2 meters; when fully fuelled, it weighed 3.370 tonnes; the propellant was a mixture of
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first stage was 5.5 metres long and had a diameter of 2 metres; when fully fuelled, it weighed 9.85 tonnes; the propellant was a mixture of
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The following planned flights were cancelled and replaced by tests of the Europa rocket (Europa 1 F7, Europa 1 F6/1 and Europa 1 F6/2).
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On 18 December 1966, a second launch took place. It reached an apogee of 55 km and was considered successful.
445:. Guidance was lost at T+62s, with the rocket reaching an apogee of 10 km. It was considered a half success. 452: 216: 322: 309: 165: 456: 383: 360: 124: 391: 372: 235: 139: 472: 314: 304: 296: 442: 292: 720: 368: 600: 387: 500: 438: 533: 633: 577: 390:. It was powered by an engine that produced 23.33 kN of thrust and had a 344:
stage was active. The Italian made Europa nose fairing was also tested.
26: 663: 288: 274: 434: 367:(UDMH). It was powered by a four-nozzle engine that produced 220 459:. Reaching an apogee of 10 km if failed due to a cabling issue. 433:
On 27 November 1966, a first launch was conducted at the
252: 244: 234: 222: 211: 203: 195: 187: 179: 171: 163: 148: 138: 130: 119: 111: 103: 95: 90: 78: 73: 65: 57: 49: 41: 36: 291:. It was the largest rocket ever launched in 8: 19: 451:On 25 October 1967, Core was launched from 319:European Launcher Development Organisation 317:, which was developed and produced by the 25: 18: 295:. It was primarily used for testing the 484: 396: 437:missile range and launch facility at 321:, the predecessor to the present day 7: 690: 688: 686: 684: 682: 680: 563: 561: 559: 557: 555: 553: 551: 494: 492: 490: 488: 14: 411: 399: 336:first stage was active. For the 732:Space launch vehicles of France 365:unsymmetrical dimethylhydrazine 1: 207:2,760 kg (6,080 lb) 199:3,370 kg (7,430 lb) 526:"Cora experimental rockets" 394:(in vacuum) of 310 seconds. 226:23.3 kN (5,200 lb 191:610 kg (1,340 lb) 748: 340:version the second German 287:was a French experimental 175:3.36 m (11.0 ft) 16:French experimental rocket 654:Wade, Mark (2016-12-28). 624:Wade, Mark (2016-12-28). 418:Coralie 1st stage diagram 271: 267: 86: 24: 313:) of the multinational 524:Jacques Serra, Jean. 406:Cora 1 stages diagram 323:European Space Agency 183:2 m (79 in) 91:First stage – Coralie 727:Experimental rockets 371:of thrust and had a 695:Capdevila, Didier. 605:Gunter's Space Page 580:on 28 December 2016 536:on 14 November 2012 505:Gunter's Space Page 31:Cora rocket diagram 21: 457:Nouvelle-Aquitaine 384:nitrogen tetroxide 361:nitrogen tetroxide 599:Gunter D, Krebs. 530:Rockets in Europe 499:Gunter D, Krebs. 282: 281: 739: 711: 710: 708: 707: 692: 675: 674: 672: 671: 662:. 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Archived from 521: 515: 514: 512: 511: 496: 415: 403: 392:specific impulse 373:specific impulse 332:only the French 275:edit on Wikidata 236:Specific impulse 140:Specific impulse 29: 22: 747: 746: 742: 741: 740: 738: 737: 736: 717: 716: 715: 714: 705: 703: 694: 693: 678: 669: 667: 653: 652: 648: 639: 637: 623: 622: 618: 609: 607: 598: 597: 593: 583: 581: 567: 566: 549: 539: 537: 523: 522: 518: 509: 507: 498: 497: 486: 481: 469: 426: 419: 416: 407: 404: 350: 278: 263: 259: 256:Aerozine 50 / N 229: 204:Propellant mass 164:Second stage – 159: 155: 32: 17: 12: 11: 5: 745: 743: 735: 734: 729: 719: 718: 713: 712: 676: 646: 616: 591: 547: 516: 483: 482: 480: 477: 476: 475: 468: 465: 461: 460: 449: 446: 443:French Algeria 425: 424:Launch history 422: 421: 420: 417: 410: 408: 405: 398: 349: 346: 293:Western Europe 280: 279: 272: 269: 268: 265: 264: 261: 257: 254: 250: 249: 246: 242: 241: 238: 232: 231: 227: 224: 223:Maximum thrust 220: 219: 213: 209: 208: 205: 201: 200: 197: 193: 192: 189: 185: 184: 181: 177: 176: 173: 169: 168: 161: 160: 157: 153: 150: 146: 145: 142: 136: 135: 132: 131:Maximum thrust 128: 127: 121: 117: 116: 113: 109: 108: 105: 101: 100: 97: 93: 92: 88: 87: 84: 83: 80: 76: 75: 74:Launch history 71: 70: 67: 63: 62: 59: 55: 54: 51: 47: 46: 43: 39: 38: 34: 33: 30: 15: 13: 10: 9: 6: 4: 3: 2: 744: 733: 730: 728: 725: 724: 722: 702: 701:Capcom Espace 698: 691: 689: 687: 685: 683: 681: 677: 666:on 2016-12-28 665: 661: 657: 650: 647: 636:on 2016-12-28 635: 631: 627: 620: 617: 606: 602: 595: 592: 579: 575: 571: 564: 562: 560: 558: 556: 554: 552: 548: 535: 531: 527: 520: 517: 506: 502: 495: 493: 491: 489: 485: 478: 474: 473:Europa Rocket 471: 470: 466: 464: 458: 454: 450: 447: 444: 440: 436: 432: 431: 430: 423: 414: 409: 402: 397: 395: 393: 389: 385: 381: 376: 374: 370: 366: 362: 358: 353: 348:Configuration 347: 345: 343: 339: 335: 331: 326: 324: 320: 316: 315:Europa Rocket 312: 311: 306: 302: 298: 294: 290: 286: 276: 270: 266: 255: 251: 247: 243: 239: 237: 233: 225: 221: 218: 214: 210: 206: 202: 198: 194: 190: 186: 182: 178: 174: 170: 167: 162: 151: 147: 143: 141: 137: 133: 129: 126: 122: 118: 114: 110: 106: 102: 98: 94: 89: 85: 81: 77: 72: 68: 64: 60: 56: 52: 48: 44: 40: 35: 28: 23: 704:. Retrieved 700: 668:. Retrieved 664:the original 659: 649: 638:. Retrieved 634:the original 629: 619: 608:. Retrieved 604: 594: 582:. Retrieved 578:the original 573: 568:Wade, Mark. 538:. Retrieved 534:the original 529: 519: 508:. Retrieved 504: 462: 427: 379: 377: 356: 354: 351: 341: 337: 333: 329: 327: 308: 305:third stages 300: 284: 283: 697:"Tirs Cora" 660:Astronautix 630:Astronautix 574:Astronautix 453:Biscarrosse 388:Aerozine-50 115:9.85 tonnes 61:16.5 tonnes 721:Categories 706:2023-08-27 670:2023-07-31 640:2023-07-31 626:"Europa-2" 610:2023-07-31 510:2023-07-30 479:References 253:Propellant 212:Powered by 196:Gross mass 188:Empty mass 149:Propellant 120:Powered by 112:Gross mass 439:Hammaguir 245:Burn time 656:"Astris" 601:"Europa" 584:27 April 540:27 April 467:See also 328:For the 180:Diameter 152:UDMH / N 104:Diameter 50:Diameter 357:Coralie 334:Coralie 301:Coralie 125:Vexin A 82:Retired 570:"Cora" 501:"Cora" 380:Astris 342:Astris 338:Cora 2 330:Cora 1 310:Astris 303:) and 297:second 289:rocket 217:Astris 172:Height 166:Astris 134:220 kN 107:2.01 m 96:Height 79:Status 66:Stages 53:2.01 m 45:11.5 m 42:Height 435:CIEES 273:[ 248:330 s 240:310 s 144:280 s 99:5.5 m 586:2018 542:2018 386:and 378:The 363:and 355:The 285:Cora 58:Mass 37:Size 20:Cora 723:: 699:. 679:^ 658:. 628:. 603:. 572:. 550:^ 528:. 503:. 487:^ 455:, 441:, 369:KN 325:. 215:1 123:4 709:. 673:. 643:. 613:. 588:. 544:. 513:. 307:( 299:( 277:] 262:4 260:O 258:2 230:) 228:f 158:4 156:O 154:2 69:2

Index


Vexin A
Specific impulse
Astris
Astris
Specific impulse
edit on Wikidata
rocket
Western Europe
second
third stages
Astris
Europa Rocket
European Launcher Development Organisation
European Space Agency
nitrogen tetroxide
unsymmetrical dimethylhydrazine
KN
specific impulse
nitrogen tetroxide
Aerozine-50
specific impulse
Cora 1 stages diagram
Coralie 1st stage diagram
CIEES
Hammaguir
French Algeria
Biscarrosse
Nouvelle-Aquitaine
Europa Rocket

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