Knowledge (XXG)

Rus-M

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3046: 381:. The second variant would add two additional cores, and allow the strapon boosters to detach earlier in flight, boosting payload capacity to 35 tons. Version 3 would use stretched tanks on the booster cores, increasing payload again to 50 tons. Version 4 would fly with only a single core, and a Soyuz 2-derived upper stage. 341:
emphasized that the launcher design is to be extremely reliable; safe abort options for crewed vehicles must be available at any stage of flight, and vehicle departure from the launch pad must be guaranteed for the case of an emergency during an early stage of the launch sequence. The launcher was
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The first version of the rocket was to use three first stage cores, inseparably bolted together, with an RD-0146 powered second stage. It would have been able to lift a cargo or satellite payload of 23.8 tons to a 200-km, 51.7-degree circular orbit, a crew vehicle of 18.8 tons to a 135 by 400-km
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In 2009, Roscomos published the specifications for a Rus-M launch vehicle. Several variants of the Rus-M were later proposed, creating a family of similar launch vehicles. In spring of 2009, TsSKB-Progress won a government contract to develop a new launcher for Russia's human space program. The
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This Template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future
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Four variants of Rus-M were planned for development. Each version would use a variable number of common cores as the first stage and boosters, each powered by a single
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Symbol indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)
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planned to provide a basis for a future heavy launcher capable to carry a payload of 50—60 tons, as well as for a super-heavy design lifting 130—150 tons.
297:) was a proposed launcher design which was intended to become Russia's main launch vehicle for crewed spaceflight after 2018, and an integral part of the 2990: 392:
was responsible for overall project leadership, system integration, second stage development and production. First stage development was to be led by
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was to provide the rocket's flight control system. After Rus-M was ultimately canceled in 2011 after falling victim to the
374: 508: 312:, beginning in 2009. The program was halted in October 2011, restarted in 2012 and finally cancelled in August 2015. 2940: 2215: 1616: 1579: 1286: 40: 2945: 2935: 1747: 1569: 1254: 357:
rocket engine burning kerosene and liquid oxygen. Two upper stages were planned. The first would have used four
2607: 1383: 412:, became the successor to Rus-M after Rus-M's cancelation and Irtysh surviving Roscosmos budget cuts in 2015. 1232: 752: 3126: 3006: 2826: 2481: 2408: 2198: 2171: 2166: 1849: 1812: 1138: 1052: 982: 904: 788: 690: 2870: 2737: 2503: 2356: 1948: 1866: 1004: 852: 408:, TsSKB Progress disclosed the existence of the Soyuz-5 rocket concept in 2013. Soyuz-5, later renamed 2782: 2642: 2112: 669: 147: 3060: 2513: 2324: 1715: 1710: 1705: 1465: 1460: 1187: 820: 378: 2314: 2257: 1943: 1700: 1648: 325:, and preliminary design of the vehicle was expected to be submitted to the Russian space agency 302: 2533: 2573: 2538: 2528: 2848: 2423: 1764: 1643: 919: 3132: 3097: 2821: 2403: 2398: 2334: 2070: 2065: 2055: 1805: 1800: 1795: 1790: 1785: 1780: 1722: 1668: 1574: 1554: 1455: 1420: 1192: 1175: 1170: 977: 899: 894: 830: 783: 762: 729: 366: 290: 246: 194: 2930: 2841: 2622: 2351: 2319: 2085: 2080: 2075: 1594: 1499: 1249: 997: 847: 757: 421: 409: 405: 401: 298: 112: 2799: 2617: 2474: 2469: 2464: 2459: 2361: 2060: 2048: 1526: 1440: 1106: 857: 778: 676: 397: 393: 389: 351: 309: 54: 44: 3177: 3065: 2858: 2853: 2662: 2657: 2652: 2612: 2329: 2304: 2250: 2245: 2235: 2230: 2225: 2107: 2102: 1931: 1631: 1626: 1514: 1410: 1371: 1366: 1356: 1346: 1336: 1326: 1321: 1316: 1311: 1306: 1301: 1296: 1291: 1202: 1062: 825: 638: 3109: 2742: 2730: 2725: 2720: 2454: 2393: 2299: 2240: 2220: 1876: 1871: 1737: 1621: 1445: 1361: 1351: 1341: 1331: 1197: 1057: 889: 322: 26: 3155: 2713: 2701: 2696: 2691: 2437: 2294: 2210: 2161: 1938: 1926: 1916: 1911: 1609: 1604: 1589: 1393: 1279: 1274: 1227: 1222: 933: 815: 447: 2975: 2895: 2767: 2762: 2757: 2752: 2747: 2708: 2684: 2679: 2674: 2669: 2543: 2523: 2119: 2028: 2023: 2018: 2013: 2008: 2003: 1921: 1732: 1658: 1584: 1564: 1504: 1487: 1482: 1477: 1403: 1398: 1388: 1269: 1259: 1182: 1143: 1024: 722: 717: 712: 695: 633: 584: 489: 609: 3091: 2907: 2890: 2814: 2809: 2777: 2772: 2647: 2583: 2578: 2568: 2563: 2558: 2518: 2508: 2491: 2428: 2344: 2339: 2203: 2191: 2181: 2129: 2038: 1906: 1881: 1859: 1757: 1752: 1653: 1531: 1242: 1237: 1207: 1148: 1047: 1019: 970: 965: 924: 840: 835: 808: 798: 700: 673: 338: 326: 3045: 2442: 938: 530:"Theses of the Speech Made by Roscosmos Head Anatoly Perminov at IAC-2009" 468: 2912: 2900: 2885: 2880: 2831: 2787: 2637: 2600: 2595: 2590: 2496: 2486: 2418: 2413: 2386: 2366: 2186: 2176: 2097: 2092: 2043: 2033: 1901: 1854: 1837: 1832: 1827: 1822: 1817: 1727: 1695: 1683: 1678: 1673: 1599: 1559: 1536: 1450: 1435: 1425: 1264: 1155: 1075: 1029: 1014: 987: 914: 909: 882: 877: 803: 793: 734: 365:. The second option would have been a kerosene fueled stage common with 3138: 2875: 2804: 2794: 2632: 2553: 2548: 2381: 2376: 2371: 2156: 1998: 1993: 1988: 1983: 1978: 1973: 1968: 1963: 1958: 1953: 1896: 1891: 1886: 1638: 1472: 1165: 1160: 1009: 960: 955: 950: 872: 867: 862: 707: 358: 227: 276: 3103: 3035: 3030: 3025: 3020: 2627: 2309: 2282: 2151: 1742: 1519: 354: 175: 2865: 2836: 2447: 2146: 1690: 1415: 1217: 992: 943: 3070: 2277: 2272: 2267: 2262: 2141: 1509: 1378: 211: 2979: 1079: 642: 2287: 2136: 263: 259: 207: 469:"РКЦ "Прогресс": проект ракеты "Русь-М" окончательно закрыт" 93:
233,000–1,440,000 kg (514,000–3,175,000 lb)
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Canceled Russian proposal for a crewed launch vehicle
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Archived from 255: 245: 233: 222: 217: 203: 193: 181: 170: 165: 153: 143: 135: 130: 118: 110: 105: 97: 89: 81: 73: 68: 60: 50: 36: 448:"Replacement for Soyuz rocket canned by Russia" 610:"Russia's new-generation rocket gets go ahead" 505:"Russia Reveals Vision for Manned Spaceflight" 2991: 1091: 654: 122:6,500–50,000 kg (14,300–110,200 lb) 8: 19: 2998: 2984: 2976: 1098: 1084: 1076: 661: 647: 639: 25: 18: 603: 601: 585:"Launch vehicle for the PPTS spacecraft" 439: 424: – Russian rocket, in development 578: 576: 574: 572: 7: 1123:Comparison of orbital launch systems 428:Comparison of orbital launch systems 337:Safety requirements put forward by 85:3.5 m (11 ft) (Main Core) 634:Launch vehicle for PPTS spacecraft 14: 556:"The Bear's stars shine brighter" 363:Chemical Automatics Design Bureau 3044: 3189:Space launch vehicles of Russia 3184:Expendable space launch systems 2951:Super heavy-lift launch vehicle 507:. IEEE Spectrum. Archived from 301:being developed to replace the 1118:List of orbital launch systems 1041:Cancelled (no launch attempts) 361:hydrolox engines developed by 1: 554:Coppinger, Rob (2009-08-11). 450:. Spaceflight Now. 2011-10-07 308:Rus-M was being developed by 185:4.15 MN (930,000 lb 375:geostationary transfer orbit 237:98.1 kN (22,100 lb 3007:RD-170 rocket engine family 503:Zak, Anatoly (2009-08-20). 251:463 s (4.54 km/s) 199:338 s (3.31 km/s) 3205: 2941:Medium-lift launch vehicle 3042: 2959: 2946:Heavy-lift launch vehicle 2936:Small-lift launch vehicle 1113: 471:. RIA Novosti. 2015-08-18 294: 273: 269: 161: 126: 77:61.1 m (200 ft) 24: 321:project was featured in 3076:Staged combustion cycle 404:, and competition with 1107:Orbital launch systems 558:. Flight International 490:"Rus-M launch vehicle" 612:. RussianSpaceWeb.com 608:Zak, Anatoly (2016). 587:. RussianSpaceWeb.com 583:Zak, Anatoly (2009). 3133:Antares (200-series) 148:Vostochny Cosmodrome 31:Rus-M Design Concept 3149:Cancelled proposals 379:geostationary orbit 373:orbit, 7.0 tons to 21: 2113:v1.2 "Full Thrust" 511:on August 25, 2009 3171: 3170: 2973: 2972: 1073: 1072: 323:MAKS 2009 Airshow 284: 283: 61:Country of origin 3196: 3085:Historic rockets 3048: 3000: 2993: 2986: 2977: 2822:Universal Rocket 1193:Falcon 9 Block 5 1100: 1093: 1086: 1077: 663: 656: 649: 640: 621: 620: 618: 617: 605: 596: 595: 593: 592: 580: 567: 566: 564: 563: 551: 545: 544: 542: 541: 526: 520: 519: 517: 516: 500: 494: 493: 486: 480: 479: 477: 476: 465: 459: 458: 456: 455: 444: 377:and 4.0 tons to 329:by August 2010. 296: 277:edit on Wikidata 247:Specific impulse 195:Specific impulse 29: 22: 3204: 3203: 3199: 3198: 3197: 3195: 3194: 3193: 3174: 3173: 3172: 3167: 3144: 3120:Current rockets 3115: 3080: 3049: 3040: 3009: 3004: 2974: 2969: 2955: 2931:Sounding rocket 2919: 1769: 1543: 1127: 1109: 1104: 1074: 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417: 414: 398:NPO Avtomatiki 394:Makeev KB Mash 390:TsSKB Progress 386: 383: 347: 344: 334: 331: 317: 314: 310:TsSKB-Progress 282: 281: 274: 271: 270: 267: 266: 257: 253: 252: 249: 243: 242: 238: 235: 234:Maximum thrust 231: 230: 224: 220: 219: 215: 214: 205: 201: 200: 197: 191: 190: 186: 183: 182:Maximum thrust 179: 178: 172: 168: 167: 163: 162: 159: 158: 155: 154:Total launches 151: 150: 145: 141: 140: 137: 133: 132: 131:Launch history 128: 127: 124: 123: 120: 116: 115: 108: 107: 103: 102: 99: 95: 94: 91: 87: 86: 83: 79: 78: 75: 71: 70: 66: 65: 62: 58: 57: 55:TsSKB-Progress 52: 48: 47: 45:launch vehicle 38: 34: 33: 30: 15: 13: 10: 9: 6: 4: 3: 2: 3201: 3190: 3187: 3185: 3182: 3181: 3179: 3163: 3160: 3157: 3154: 3153: 3151: 3147: 3140: 3137: 3134: 3131: 3128: 3125: 3124: 3122: 3118: 3111: 3108: 3105: 3102: 3099: 3096: 3093: 3090: 3089: 3087: 3083: 3077: 3074: 3072: 3069: 3067: 3064: 3062: 3059: 3058: 3056: 3052: 3047: 3037: 3034: 3032: 3029: 3027: 3024: 3022: 3019: 3018: 3016: 3012: 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Retrieved 589:. Retrieved 560:. Retrieved 549: 538:. Retrieved 534:the original 524: 513:. Retrieved 509:the original 498: 484: 473:. Retrieved 463: 452:. Retrieved 442: 388: 371: 349: 336: 333:Requirements 319: 307: 286: 285: 218:Second stage 144:Launch sites 51:Manufacturer 3014:Derivatives 2211:LauncherOne 2162:Kaituozhe-1 1939:Black Arrow 1691:Orbex Prime 1590:Hyperbola-2 1555:Antares 330 1255:Kaituozhe 2 1228:Hyperbola-1 385:Development 346:Description 166:First stage 111:Payload to 41:Human-rated 3178:Categories 2216:Long March 2120:Feng Bao 1 1733:Tianlong-3 1659:New Line 1 1617:Long March 1565:Cyclone-4M 1505:Tianlong-2 1483:2.1b / STB 1478:2.1a / STA 1421:Pegasus XL 1287:Long March 1260:Kinetica 1 1183:Chollima-1 616:2021-10-25 591:2009-08-22 562:2009-08-22 540:2009-10-13 515:2009-08-22 475:2019-03-03 454:2011-10-08 434:References 352:Energomash 256:Propellant 223:Powered by 204:Propellant 171:Powered by 3092:Atlas III 2315:Paektusan 1944:Conestoga 1701:Red Dwarf 1654:New Glenn 1585:Gravity-2 1575:Epsilon S 1208:Gravity-1 1048:Tsyklon-4 339:Roscosmos 327:Roscosmos 139:Cancelled 106:Capacity 3164:(RD-180) 3158:(RD-180) 3141:(RD-180) 3135:(RD-181) 3129:(RD-191) 3112:(RD-171) 3106:(RD-151) 3100:(RD-170) 3094:(RD-180) 2859:original 2849:Vanguard 2832:Proton-K 2805:original 2653:Ablestar 2638:Terran 1 2596:original 2455:Rocket 3 2362:original 2172:original 2098:Falcon 9 2093:Falcon 1 2049:IV Heavy 1765:Zuljanah 1728:Terran R 1711:Block 1B 1696:Pallas-1 1600:Kuaizhou 1560:Bloostar 1500:Starship 1451:Shavit 2 1436:Qaem 100 1426:Proton-M 1384:Minotaur 1265:Kuaizhou 1188:Electron 1156:Ariane 6 988:Proton-K 961:original 858:original 735:Proton-M 416:See also 410:"Irtysh" 396:, while 82:Diameter 43:orbital 37:Function 3139:Atlas V 3098:Energia 2924:Classes 2795:Tsyklon 2633:Start-1 2404:Voskhod 2399:Sputnik 2335:Molniya 2320:Pilot-2 2157:Juno II 2071:Epsilon 2066:Energia 2056:Diamant 1932:Centaur 1781:Antares 1774:Retired 1723:Soyuz-7 1716:Block 2 1649:Neutron 1639:Miura 5 1473:Soyuz-2 1466:Block 1 1456:Simorgh 1233:Jielong 1161:Atlas V 1132:Current 956:Tsyklon 951:Start-1 900:Voskhod 895:Sputnik 831:Molniya 784:Energia 772:Retired 763:Yenisei 708:Soyuz-2 674:Russian 367:Soyuz-2 359:RD-0146 316:History 291:Russian 228:RD-0146 3127:Angara 3104:Naro-1 3036:RD-151 3031:RD-191 3026:RD-180 3021:RD-171 2908:Zhuque 2842:Strela 2800:R-36-O 2743:II GLV 2731:SLV-2H 2726:SLV-2G 2714:DSV-2U 2692:Burner 2628:SS-520 2623:Sparta 2591:Shavit 2482:Saturn 2443:Shtil' 2409:Vostok 2352:Polyot 2310:Naro-1 2199:Lambda 2167:Kosmos 2152:Juno I 2076:Europa 1850:Athena 1813:Ariane 1753:Zhuque 1743:Vega E 1595:Irtysh 1532:Zhuque 1250:KAIROS 1139:Angara 1063:Medium 1053:Proton 998:Strela 983:UR-500 939:Shtil' 905:Vostok 848:Polyot 789:Kosmos 758:Irtysh 691:Angara 684:Active 670:Soviet 422:Irtysh 406:Angara 355:RD-180 295:Русь-М 176:RD-180 136:Status 98:Stages 74:Height 64:Russia 3162:Rus-M 3110:Zenit 2871:Zenit 2866:VLS-1 2837:Rokot 2738:Titan 2709:Delta 2670:Agena 2618:SPARK 2504:Scout 2460:Safir 2448:Volna 2357:Soyuz 2147:H-IIB 2061:Dnepr 1949:Delta 1927:Agena 1917:SLV-3 1912:LV-3B 1867:Atlas 1441:Qased 1416:OS-M1 1218:H-IIA 1166:Ceres 1058:Light 1005:Zenit 993:Rokot 944:Volna 853:Soyuz 779:Dnepr 303:Soyuz 287:Rus-M 275:[ 101:2 - 3 20:Rus-M 3071:RP-1 2896:3SLB 2854:Vega 2783:CT-3 2768:IIIE 2763:IIID 2758:IIIC 2753:IIIB 2748:IIIA 2648:Able 2643:Thor 2544:X-2B 2534:X-3M 2524:X-2M 2438:R-29 2330:Luna 2305:N-II 2283:3SII 2182:2/2I 2142:H-II 2130:Mk I 2125:GSLV 2108:v1.1 2103:v1.0 2029:5000 2024:4000 2019:3000 2014:2000 2009:1000 2004:0100 1922:Able 1845:ASLV 1806:230+ 1748:Zero 1674:OS-M 1669:Nova 1664:NGLV 1580:Eris 1570:Deca 1515:Vega 1510:Unha 1495:SSLV 1488:2-1v 1431:PSLV 1411:Nuri 1379:LVM3 1312:3B/E 1213:GSLV 1025:3SLB 934:R-29 826:Luna 753:Amur 723:2-1v 718:2.1b 713:2.1a 672:and 212:RP-1 119:Mass 90:Mass 69:Size 3066:LOX 2891:3SL 2886:2FG 2778:23G 2773:34D 2608:SLV 2584:G-1 2579:F-1 2574:E-1 2569:A-1 2564:D-1 2559:B-1 2539:X-4 2529:X-3 2519:X-2 2509:X-1 2325:R-7 2300:N-I 2137:H-I 2039:III 1907:III 1882:E/F 1801:230 1796:130 1791:120 1786:110 1738:VLM 1706:SLS 1644:MLV 1461:SLS 1446:RS1 1372:11H 1144:1.2 1020:3SL 821:R-7 696:1.2 264:LH2 260:LOX 208:LOX 113:LEO 3180:: 3156:GX 2901:3F 2881:2M 2788:IV 2492:IB 2475:1B 2470:1A 2429:2M 2387:U2 2367:FG 2295:N1 2278:3S 2273:3H 2268:3C 2263:4S 2258:Mu 2251:4A 2246:3B 2236:2E 2231:2A 2226:1D 2204:4S 2192:3M 2086:II 2044:IV 2034:II 1902:II 1860:II 1632:12 1627:10 1610:31 1605:21 1394:IV 1367:11 1357:7A 1347:6A 1337:5B 1327:4C 1322:4B 1317:3C 1307:3A 1302:2F 1297:2D 1292:2C 1280:11 1275:1A 1223:H3 1176:1S 1149:A5 1030:3F 1015:2M 978:UR 925:2M 883:FG 878:U2 816:N1 809:3M 799:2I 730:UR 701:A5 600:^ 571:^ 369:. 305:. 293:: 226:4 174:3 2999:e 2992:t 2985:v 2913:1 2876:2 2815:3 2810:2 2702:2 2697:1 2685:D 2680:B 2675:A 2663:2 2658:1 2601:1 2554:A 2549:B 2497:V 2487:I 2465:1 2424:2 2419:K 2414:L 2382:U 2377:M 2372:L 2345:L 2340:M 2288:V 2241:3 2221:1 2187:3 2177:1 2081:I 1999:N 1994:M 1989:L 1984:J 1979:G 1974:E 1969:D 1964:C 1959:B 1954:A 1897:I 1892:H 1887:G 1877:D 1872:B 1855:I 1838:5 1833:4 1828:3 1823:2 1818:1 1758:3 1684:4 1679:2 1622:9 1537:2 1520:C 1404:C 1399:V 1389:I 1362:8 1352:7 1342:6 1332:5 1270:1 1243:3 1238:1 1171:1 1099:e 1092:t 1085:v 1010:2 971:3 966:2 920:2 915:K 910:L 873:U 868:M 863:L 841:L 836:M 804:3 794:1 662:e 655:t 648:v 619:. 594:. 565:. 543:. 518:. 492:. 478:. 457:. 289:( 279:] 262:/ 241:) 239:f 210:/ 189:) 187:f 157:0

Index


Human-rated
launch vehicle
TsSKB-Progress
LEO
Vostochny Cosmodrome
RD-180
Specific impulse
LOX
RP-1
RD-0146
Specific impulse
LOX
LH2
edit on Wikidata
Russian
Orel spacecraft
Soyuz
TsSKB-Progress
MAKS 2009 Airshow
Roscosmos
Roscosmos
Energomash
RD-180
RD-0146
Chemical Automatics Design Bureau
Soyuz-2
geostationary transfer orbit
geostationary orbit
TsSKB Progress

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