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P80 (rocket stage)

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1749: 378: 317:- it has the same 3 meter diameter and similar height to the largest segments of the booster. This allows using the same facilities and equipment at the Guiana Propellant Plant for loading the propellant and transporting the engine to the launch site. The nozzle of the P80 is also a direct evolution of the one used in Ariane 5 boosters. 324:
manufactures the main motor case loaded with fuel, performs integration of the components, and final testing. French-Italian Europropulsion manufactures the P80 motor while Regulus performs propellant loading. Aerospace Propulsion Products B.V. from
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in November 2006 followed by qualification tests in December 2007. The first launch was completed on 13 February 2012, with the first commercial launch following on 7 May 2012. Total development cost of the engine reached €76 million.
1886: 553: 454: 704: 1881: 735: 671: 2001: 262:(in the P80FW version). It was the world's largest and most powerful one-piece solid-fuel rocket engine, being replaced by the larger 517: 304: 650: 601: 1400: 307:
which burns for 114 seconds and is jettisoned at an altitude of 53 km after achieving a relative speed of 1.7 km/s.
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a wider version of the engine with increased propellant mass to 143.6 tons, for use in
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selected as the prime contractor. The first test of the P80 engine was completed at
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The manufacture process is divided among several European companies. Italian
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first stage. In 2022, an extended P120C+ version was proposed.
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P80FW is a single monolithic solid rocket motor propelled by
554:"ESA's new Vega launcher scores success on maiden flight" 673:
ESA-developed P120C solid rocket motor enters production
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Solid-fuel first-stage rocket motor used on the ESA Vega
457:. European Launch Vehicle S.p.A. P.IVA. Archived from 623:
APP Aerospace Propulsion Products B.V. (7 May 2013).
1756: 1685: 1382: 1375: 1106: 1097: 945: 764: 755: 744: 223: 215: 205: 193: 185: 177: 169: 161: 153: 148: 136: 128: 118: 110: 102: 97: 87: 82: 72: 62: 52: 274:The P80's development was led by a joint team of 602:"Vega's second success 'confirms functionality'" 484: 482: 480: 478: 476: 698: 8: 490:"Press Kit - Vega qualification flight VV01" 32: 1379: 1103: 761: 752: 705: 691: 683: 31: 181:95 tonnes (93 long tons; 105 short tons) 418: 189:88 tonnes (87 long tons; 97 short tons) 455:"Vega Launcher - Launcher Composition" 310:The engine shares specifications with 449: 447: 7: 736:Comparison of orbital rocket engines 197:3,037 kilonewtons (683,000 lb 25: 576:"Vega maiden launch goes to plan" 305:hydroxyl-terminated polybutadiene 1747: 376: 341:manufactures the engine nozzle. 173:7,330 kilograms (16,160 lb) 38: 651:"P120 C solid propellant motor" 337:and the staging skirt. French 1: 1532:RD-0202 to 0206, 0208 to 0213 427:"VEGA: 1° Stage - P80 Motor" 329:builds the igniter. Belgian 2094: 604:. Flightglobal. 9 May 2013 2042: 1745: 731: 518:"Vega Satellite Launcher" 238: 144: 44:P80 being transferred at 37: 333:produces components for 157:10.6 metres (35 ft) 1577:RD-250 to 252, 261, 262 556:. ESA. 13 February 2012 292:Centre Spatial Guyanais 165:3 metres (9.8 ft) 2053:are under development 1441:YF-20, 21, 22, 24, 25 1220:RD-107, 108, 117, 118 397:Zefiro (rocket stage) 315:solid rocket boosters 257:European Space Agency 534:on 23 September 2015 1542:RD-0216, 0217, 0235 1205:RD-0107, 0108, 0110 631:on 4 September 2013 392:P120 (rocket stage) 345:Related development 46:Guiana Space Centre 34: 2078:Solid-fuel rockets 582:. 13 February 2012 384:Spaceflight portal 2060: 2059: 2002:Space Shuttle SRB 1743: 1742: 1681: 1680: 1371: 1370: 1093: 1092: 286:since 2005, with 266:on 13 July 2022. 242: 241: 83:Associated stages 63:Country of origin 16:(Redirected from 2085: 1751: 1750: 1587:RD-263, 268, 273 1518:along other LREs 1380: 1240:RD-191, 151, 181 1104: 762: 753: 707: 700: 693: 684: 677: 669: 663: 662: 657:. Archived from 647: 641: 640: 638: 636: 627:. Archived from 620: 614: 613: 611: 609: 598: 592: 591: 589: 587: 572: 566: 565: 563: 561: 550: 544: 543: 541: 539: 533: 527:. Archived from 522: 514: 508: 507: 505: 503: 494: 486: 471: 470: 468: 466: 451: 442: 441: 439: 437: 423: 386: 381: 380: 379: 335:thrust vectoring 207:Specific impulse 149:1 stage – P80FW 132:13 February 2012 42: 35: 21: 2093: 2092: 2088: 2087: 2086: 2084: 2083: 2082: 2063: 2062: 2061: 2056: 2038: 1759: 1752: 1748: 1739: 1677: 1567:RD-0255 to 0257 1562:RD-0243 to 0245 1424: 1413: 1409: 1403: 1391: 1367: 1108: 1099: 1089: 953: 947: 941: 772: 766: 747: 740: 727: 725:launch vehicles 711: 681: 680: 670: 666: 661:on 4 June 2019. 649: 648: 644: 634: 632: 622: 621: 617: 607: 605: 600: 599: 595: 585: 583: 574: 573: 569: 559: 557: 552: 551: 547: 537: 535: 531: 520: 516: 515: 511: 501: 499: 492: 488: 487: 474: 464: 462: 461:on 4 March 2016 453: 452: 445: 435: 433: 425: 424: 420: 415: 382: 377: 375: 372: 352: 347: 301: 272: 200: 186:Propellant mass 120: 48: 28: 23: 22: 15: 12: 11: 5: 2091: 2089: 2081: 2080: 2075: 2065: 2064: 2058: 2057: 2055: 2054: 2047: 2043: 2040: 2039: 2037: 2036: 2035: 2034: 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Retrieved 629:the original 618: 606:. Retrieved 596: 584:. Retrieved 580:Flightglobal 570: 558:. Retrieved 548: 536:. Retrieved 529:the original 512: 500:. Retrieved 463:. Retrieved 459:the original 434:. Retrieved 421: 402:Solid rocket 353: 319: 309: 302: 273: 255:used on the 253:rocket motor 251:first-stage 244: 243: 129:First flight 121:(stage only) 53:Manufacturer 29: 2049:Engines in 1696:RD-109, 119 1634:RD-864, 869 1619:RD-854, 861 1582:RD-253, 275 1230:RD-170, 171 608:16 December 586:16 December 560:16 December 327:Netherlands 260:Vega rocket 219:114 seconds 211:280 seconds 137:Last flight 88:Derivatives 18:P80 (stage) 2067:Categories 1436:YF-1, 2, 3 1384:Hypergolic 1356:Rutherford 1075:Prometheus 1037:Archimedes 675:April 2022 635:14 January 413:References 249:solid-fuel 224:Propellant 178:Gross mass 170:Empty mass 1977:Castor 30 1857:Zefiro 40 1852:Zefiro 23 1793:SpaB-140C 1190:NK-33, 44 1100:cryogenic 946:Methalox 765:Hydrolox 757:Cryogenic 228:Aluminium 216:Burn time 119:Successes 1992:Orbus-21 1847:Zefiro 9 1610:Ukraine 1388:Aerozine 1376:Storable 1268:Ukraine 1210:RD-0110R 1107:Kerolox 436:14 April 370:See also 360:Ariane 6 339:Herakles 312:Ariane 5 299:Overview 162:Diameter 2051:italics 2012:Star 48 2007:Star 37 1987:Orbus-6 1908:Israel 1842:Waxwing 1798:Europe 1790:SpaB-65 1692:Russia 1557:RD-0237 1552:RD-0236 1523:Russia 1502:Israel 1462:Europe 1306:Kestrel 1252:S1.5400 1215:RD-0124 1181:Russia 1174:SCE-200 1070:Europe 1063:RD-0169 1058:Russia 984:Longyun 977:Lingyun 895:RD-0146 889:RD-0120 880:Russia 837:Vulcain 823:Europe 746:Liquid 722:orbital 538:22 July 502:22 July 465:22 July 270:History 73:Used on 1967:AJ-60A 1932:KM-V2b 1923:Japan 1897:Salman 1863:India 1837:Topaze 1802:Mage 1 1767:China 1758:Solid 1665:TR-201 1629:RD-856 1624:RD-855 1614:RD-843 1604:S5.98M 1593:RD-270 1487:India 1481:Viking 1471:Astris 1466:Aestus 1456:YF-50D 1432:China 1341:RS-27A 1331:Merlin 1321:LR-105 1285:RD-810 1278:RD-801 1262:TEPREL 1258:Spain 1246:RD-193 1235:RD-180 1225:RD-120 1169:India 1162:Welkin 1155:YF-130 1149:YF-115 1144:YF-102 1139:YF-100 1123:China 1051:Aeon R 1044:Aeon 1 1031:Raptor 1015:YF-215 1008:YF-209 1001:TQ-15A 965:China 858:Japan 847:CE-7.5 843:India 798:YF-75D 784:China 364:Vega C 154:Height 106:Active 103:Status 2032:X-254 2027:X-248 2017:UA120 1997:Orion 1972:Algol 1957:SRB-A 1952:M-34c 1927:KM-V1 1917:RSA-3 1893:Iran 1786:FG-47 1781:FG-46 1776:FG-36 1771:FG-02 1732:XLR81 1726:RS-88 1721:Curie 1711:Gamma 1686:Other 1670:XLR81 1659:RS-88 1654:LR-91 1649:LR-87 1599:S5.92 1527:17D61 1496:Vikas 1476:Vexin 1451:YF-40 1446:YF-23 1419:, or 1399:, or 1393:UH 25 1361:XLR50 1346:RS-56 1336:RS-27 1316:LR-89 1311:LR-79 1195:RD-58 1185:NK-15 1133:TH-12 1127:TH-11 1098:Semi- 995:TQ-12 990:TQ-11 970:BF-20 935:RS-68 930:RS-25 907:BE-3U 852:CE-20 832:Vinci 816:YF-90 809:YF-79 803:YF-77 793:YF-75 788:YF-73 532:(PDF) 521:(PDF) 493:(PDF) 356:P120C 350:P120C 331:SABCA 264:P120C 247:is a 67:Italy 33:P80FW 2022:SRMU 1947:M-34 1942:M-24 1937:M-14 1912:LK-1 1902:Rafe 1887:S200 1882:S139 1832:P230 1827:P120 1760:fuel 1644:AJ10 1506:LK-4 1401:UDMH 1351:S-3D 1272:RD-8 1111:RP-1 1082:M-10 1026:BE-4 925:RL10 914:BE-7 873:LE-9 867:LE-7 862:LE-5 827:HM7B 748:fuel 720:for 716:and 637:2014 610:2015 588:2015 562:2015 540:2014 525:Avio 504:2014 467:2014 438:2019 431:Avio 354:The 322:Avio 288:Avio 282:and 280:CNES 234:1912 232:HTPB 92:P120 77:Vega 57:Avio 1982:GEM 1877:S12 1822:P80 1817:PAP 1812:P-6 1807:P-4 1707:UK 1491:PS4 1421:HNO 1417:MON 1397:MMH 1301:H-1 1296:F-1 1115:LOX 957:LOX 920:J-2 776:LOX 497:ESA 284:ASI 276:ESA 245:P80 2069:: 1872:S9 1867:S7 1415:, 1404:/ 1395:, 1390:, 1113:/ 955:/ 950:CH 774:/ 769:LH 653:. 578:. 523:. 495:. 475:^ 446:^ 429:. 278:, 124:21 114:21 1734:* 1728:* 1672:* 1661:* 1426:) 1423:3 1412:4 1410:O 1408:2 1406:N 1386:( 1117:) 1109:( 959:) 952:4 948:( 778:) 771:2 767:( 706:e 699:t 692:v 639:. 612:. 590:. 564:. 542:. 506:. 469:. 440:. 230:- 201:) 199:f 20:)

Index

P80 (stage)

Guiana Space Centre
Avio
Italy
Vega
P120
Specific impulse
Aluminium
HTPB
solid-fuel
rocket motor
European Space Agency
Vega rocket
P120C
ESA
CNES
ASI
Avio
Centre Spatial Guyanais
hydroxyl-terminated polybutadiene
Ariane 5
solid rocket boosters
Avio
Netherlands
SABCA
thrust vectoring
Herakles
P120C
Ariane 6

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