35:
3245:
433:
project, he originally intended to use multiple UR-200 modules as a first stage. When this concept proved not viable, and the multi-body that was finally used was settled on, they had to search for new propulsion on the first stage. For the second stage, they adapted the UR-200 first stage's. It
434:
needed new tanks to match the first stage, but most of the rest could be adapted. The engines had to be started in the air and had to get longer nozzles, optimized for vacuum operation. Both of this features were demonstrated on the RD-0206, and were readily adapted. They also received a
474:
by uprating them slightly and significantly increasing the burning time. For the third stage, the UR-200 second stage was adapted -again, with the same 4.1m tanking as the first and second stages- and the RD-0205 module with an RD-0206 and an RD-0207
411:. The RD-0204 only difference to the RD-0203 was that it included a heat exchanger to heat the pressurant gases for the first stage tank. The RD-0206 was very similar to the RD-0204, but its nozzle was vacuum optimized and had a fixed nozzle. The
608:): The second staged combustion rocket in the world, and the first hypergolic. It used an oxidizer rich preburner and had a thrust of 559.00 kN (125,670 lbf). Propulsion of the UR-200 first stage.
449:
When the UR-500 proved to be too big as an ICBM, the application of the vehicle as a weapon was cancelled. But it could be adapted as a heavy launch vehicle that could perform important missions for the
466:. For this new missions, it would not need to comply with ICBM specification standards, but would need at least a third stage. The second stage was enlarged, and the RD-0208/9 were revised as the
3583:
3578:
364:
to develop the propulsion. They decided to use the same basic block for both the first and second stage. But to achieve the required performance, Kosberg had to develop a
593:
The basic engine has been used for the UR-200 first and second stages, the UR-500 second stage and the Proton second and third stages. Each variation is as follows:
3382:
3573:
1466:"RD0208, RD0209 Launch Vehicle Proton (8K82H-4 two stages). RD0210, RD0211, RD0212 (RD0213, RD0214) Launch Vehicle Proton (8K82K, 8K82KM three stages)"
2200:
3377:
614:: Slight variation of the RD-0203 that included a heat exchanger for heating the tank pressurizant gases. Propulsion of the UR-200 first stage.
383:
To simplify design and manufacture, the engine would be used both on the first and the second stages. The first stage would use a module - the
2162:
1537:
2231:
1734:"KBKHA LIQUID ROCKET ENGINES, WHICH ENSURED THE SUCCESSFUL REALIZATION OF THE ADVANCED SPACE PROGRAMS (FOR THE FIRST TIME IN THE WORLD)"
696:, it is the same as RD-0210, but with a heat exchanger like the RD-0209. Used on the second stage of the Proton-K and Proton-M rockets.
34:
3497:
3568:
361:
2097:
905:
500:
365:
308:
166:
2896:
920:
304:
148:
3372:
3367:
3362:
2986:
2079:
1465:
2050:
1934:
1905:
1876:
1847:
1818:
1754:
646:): Evolution of the RD-0203, with vacuum optimized nozzle and air start capability. Used on the second stage of the UR-500.
446:
were born. In a parallel case with the RD-0203/4, the RD-0209 was a version of the RD-0208 that included a heat exchanger.
3588:
2193:
451:
2021:
1992:
1963:
1786:
1586:
2115:
723:
Some of these engines were bundled into modules of multiple engines. The relevant modules and auxiliary engines are:
3517:
2851:
2570:
2532:
734:
Index: 8D45): A module comprising three RD-0203 and a single RD-0204. Propulsion module of the UR-200 first stage.
491:
vernier engine. The RD-0213 was a RD-0206 brought to RD-0211/12 standards, and the RD-0214 was a revised RD-0207.
369:
1413:
81:
2912:
2241:
902:
127:
2178:
3253:
2479:
2472:
2332:
2186:
582:
3337:
3206:
2976:
2966:
2657:
2639:
519:
332:
320:
3527:
3522:
3472:
3392:
3352:
3347:
3342:
3216:
2991:
2941:
2879:
2327:
1733:
423:
and was cancelled in favor of the latter, it did have a few test launches and thus was a proven design.
2170:
3492:
3487:
3482:
3477:
3467:
2901:
2213:
909:
293:
137:
3502:
3322:
3022:
2892:
2577:
2217:
1541:
678:, it is an evolution of the RD-0208. Used on the second stage of the Proton-K and Proton-M rockets.
574:
3317:
563:
761:
Index: 8D49): Also known as the RD-473, it is a propulsion module comprising one RD-0213 and an
3397:
344:
2134:
1484:
3447:
3427:
2546:
2539:
1385:
1371:
980:
972:
964:
956:
765:
748:
711:
629:
476:
435:
412:
404:
312:
210:
2846:
2264:
1395:
1262:
1255:
1248:
458:
was born. This allowed
Chelomey to pitch it as a competitor, along the UR-700 project, of
267:
102:
2080:"RD-0203, RD-0204, RD-0205, RD-0206, RD-0207. Intercontinental ballistic missile UR-200"
2821:
2801:
2796:
2791:
2415:
2252:
2220:
2101:
459:
420:
358:
660:): Same as RD-0208, but with a heat exchanger. Used on the second stage of the UR-500.
3562:
2826:
2610:
2526:
2452:
2271:
2209:
1646:
1419:
289:
1696:
1671:
1621:
2083:
559:
design, and a lander which was sent the first pictured from the surface of Venus.
1469:
2916:
2883:
2816:
2811:
2806:
2058:
2029:
2000:
1971:
1942:
1913:
1884:
1855:
1826:
1794:
1762:
544:
bus, and the lander was the first man made object to reach the surface of Mars.
463:
1416:- A space hardware manufacturing company that makes the RD-0210/11 and RD-0212.
510:
On 15 September 1968 the RD-0210, RD-0211 and the RD-0212 module launched the
427:
1513:
507:, and was also the first staged combustion engine with storable propellants.
2951:
1559:
768:. Propulsion module of the third stage of the Proton-K and Proton-M rockets.
1594:
2119:
419:
vernier engine. While the UR-200 project was in direct competition to the
3412:
3407:
3327:
3312:
3297:
3001:
2705:
548:
541:
526:
522:, that sent the first alive organisms around the moon and back to Earth.
380:, and it used a different propellant mix with significantly less thrust.
200:
3542:* Different versions of the engine use different propellant combinations
3507:
3332:
3307:
3302:
3062:
3057:
3052:
3047:
3042:
3037:
3032:
2971:
2747:
2710:
2700:
2695:
2669:
2558:
2445:
2390:
2384:
2118:. Khrunichev State Research and Production Space Center. Archived from
2100:. Khrunichev State Research and Production Space Center. Archived from
1381:
1367:
862:
845:
762:
745:
504:
377:
316:
112:
17:
710:): Variation of the RD-0210/11, optimized for vacuum expansion and no
3462:
3196:
3191:
3160:
3129:
3124:
3119:
3114:
3109:
3099:
3088:
3082:
3077:
3072:
3067:
3011:
2961:
2836:
2780:
2773:
2757:
2741:
2735:
2730:
2725:
2720:
2715:
2650:
2644:
2634:
2510:
2503:
2342:
2293:
1401:
1241:
1234:
1227:
1220:
1213:
628:): Variation of the RD-0203/4, optimized for vacuum expansion and no
578:
556:
533:
511:
455:
430:
351:
347:
263:
52:
3512:
3452:
3281:
3276:
3271:
3266:
3227:
3221:
3165:
3154:
3144:
3094:
2946:
2936:
2888:
2856:
2841:
2831:
2690:
2685:
2680:
2628:
2622:
2496:
2490:
2485:
2465:
2430:
2425:
2402:
2379:
2347:
2311:
2304:
2298:
2288:
2283:
1407:
714:. Used on the RD-0212 propulsion module of the Proton third stage.
552:
438:
gimbaling system, to have better control during launch. Thus, the
373:
70:
284:
Index: 8D411K) is also known as the RD-465. It and its twin, the
3149:
3139:
2931:
2767:
2606:
2521:
2420:
2409:
2368:
2362:
2357:
2322:
758:
741:
731:
703:
685:
667:
653:
639:
621:
601:
537:
515:
354:
281:
48:
2182:
2098:"RD-0210/0211 (8D411 K/8D412K) Liquid-propellant rocket engine"
3442:
3437:
3432:
3422:
567:
1737:
577:, the third module launched of the ISS and the center of the
2157:
1622:"Birth of Proton: The Iconic Rocket That Almost Wasn't"
2171:
Khrunichev State
Research and Production Space Center
744:
Index: 8D46): A module comprising an RD-0206 and an
376:
had designed a staged combustion engine before, the
3252:
3181:
2878:
2871:
2602:
2593:
2441:
2260:
2251:
2240:
257:
249:
241:
233:
228:
220:
209:
198:
190:
185:
177:
172:
162:
154:
133:
126:
118:
108:
95:
87:
77:
66:
58:
44:
1404:- Used the RD-0202 and RD-0205 propulsion modules.
479:was given an overhaul. The new module, - known as
3584:Rocket engines using the staged combustion cycle
2116:"RD-0212 (8D49) Liquid-propellant rocket engine"
1728:
1726:
1724:
1722:
1720:
1718:
1716:
1615:
1613:
1611:
327:is a fixed nozzle variation that is used on the
1460:
1458:
1456:
1454:
368:engine, a then extremely aggressive feat. Only
1452:
1450:
1448:
1446:
1444:
1442:
1440:
1438:
1436:
1434:
2194:
8:
1813:
1811:
1781:
1779:
1749:
1747:
1507:
1505:
1503:
1501:
529:the first space station to orbit the Earth.
27:
1553:
1551:
1540:. Voronezh Mechanical Plant. Archived from
1410:- The RD-0210/11 and RD-0212 design bureau.
3579:Rocket engines using hypergolic propellant
2875:
2599:
2257:
2248:
2201:
2187:
2179:
1581:
1579:
555:. It consisted of an orbiter based on the
319:lineage. They are the engines used on the
33:
311:cycle. They have single nozzle, possess
771:
751:. Propulsion of the UR-200 second stage.
1430:
1485:"Le troisième étage du lanceur Proton"
562:On 20 November 1998 a Proton launched
415:task was delegated to the four nozzle
97:
26:
2135:"Le deuxième étage du lanceur Proton"
547:On 8 June 1975 a Proton launched the
532:On 19 May 1971 a Proton launched the
7:
2232:Comparison of orbital rocket engines
923:propellant with an O/F ratio of 2.6
503:engine in the world, only after the
395:, while the upper stage would use a
315:and are the latest evolution in the
540:. The orbiter was identical to the
3574:Rocket engines of the Soviet Union
632:. Used on the UR-200 second stage.
573:On 12 July 2000 a Proton launched
525:On 19 April 1971 a Proton orbited
25:
3243:
1001:575.5 kN (129,400 lbf)
426:When Chelomey started his super
1016:582 kN (131,000 lbf)
931:14.7 MPa (2,130 psi)
906:oxidizer rich staged combustion
309:oxidizer rich staged combustion
167:Oxidizer Rich Staged combustion
1398:- uses RD-0210/11 and RD-0212.
1205:550 kilograms (1,210 lb)
1148:3,008 mm (118.4 in)
1027:500 kN (110,000 lbf)
1024:500 kN (110,000 lbf)
1013:582 kN (131,000 lbf)
1010:582 kN (131,000 lbf)
1007:570 kN (130,000 lbf)
1004:570 kN (130,000 lbf)
998:559 kN (126,000 lbf)
995:559 kN (126,000 lbf)
403:main engine plus an auxiliary
205:14.7 MPa (2,130 psi)
194:582 kN (131,000 lbf)
1:
3028:RD-0202 to 0206, 0208 to 0213
2137:(in French). Kosmonavtika.com
1487:(in French). Kosmonavtika.com
1202:566 kilograms (1,248 lb)
1199:566 kilograms (1,248 lb)
1196:540 kilograms (1,190 lb)
1193:540 kilograms (1,190 lb)
581:portion of the station - the
499:The RD-0203/4 was the second
1145:2,327 mm (91.6 in)
1142:2,327 mm (91.6 in)
1139:2,327 mm (91.6 in)
1136:2,327 mm (91.6 in)
928:Combustion Chamber Pressure
237:2,327 mm (91.6 in)
1188:381 kilograms (840 lb)
1185:381 kilograms (840 lb)
1177:1,470 mm (58 in)
253:566 kg (1,248 lb)
3605:
2163:Voronezh Mechanical Plant
1174:1,470 mm (58 in)
1171:1,470 mm (58 in)
1168:1,470 mm (58 in)
1165:1,470 mm (58 in)
1162:1,470 mm (58 in)
773:RD-0210 Family of Engines
245:1,470 mm (58 in)
73:, Yankel I. Guerchkovitch
3538:
3241:
2227:
2055:Encyclopedia Astronautica
2026:Encyclopedia Astronautica
1997:Encyclopedia Astronautica
1968:Encyclopedia Astronautica
1939:Encyclopedia Astronautica
1910:Encyclopedia Astronautica
1881:Encyclopedia Astronautica
1852:Encyclopedia Astronautica
1823:Encyclopedia Astronautica
1791:Encyclopedia Astronautica
1759:Encyclopedia Astronautica
1647:"Proton/UR-500/8k82/SL-9"
1591:Encyclopedia Astronautica
1560:"UR-200 / 8K81 / SS-X-10"
1414:Voronezh Mechanical Plant
1355:
930:
901:
838:
262:
82:Voronezh Mechanical Plant
32:
3569:Rocket engines of Russia
1159:890 mm (35 in)
1156:890 mm (35 in)
566:the first module of the
357:project, they requested
3073:RD-250 to 252, 261, 262
2082:. KBKhA. Archived from
1736:. KBKhA. Archived from
1701:www.russianspaceweb.com
1676:www.russianspaceweb.com
1672:"Proton's second stage"
1651:www.russianspaceweb.com
1626:www.russianspaceweb.com
1564:www.russianspaceweb.com
1518:www.russianspaceweb.com
1468:. KBKhA. Archived from
1131:1.8 m (71 in)
1128:1.8 m (71 in)
583:Russian Orbital Segment
387:- that comprised three
1697:"Proton's third stage"
1538:"Liquid Rocket Engine"
520:free return trajectory
3549:are under development
2937:YF-20, 21, 22, 24, 25
2716:RD-107, 108, 117, 118
692:): Also known as the
674:): Also known as the
413:thrust vector control
3589:KBKhA rocket engines
399:module comprising a
3038:RD-0216, 0217, 0235
2701:RD-0107, 0108, 0110
1797:on January 13, 2003
1021:Thrust (Sea Level)
774:
29:
2032:on August 26, 2002
2003:on August 26, 2002
1974:on August 26, 2002
1472:on 15 August 2015.
836:Propulsion Module
772:
483:- consisted of an
323:second stage. The
128:Liquid-fuel engine
28:RD-0210 (РД-0210)
3556:
3555:
3498:Space Shuttle SRB
3239:
3238:
3177:
3176:
2867:
2866:
2589:
2588:
2133:Pillet, Nicolas.
1740:on 24 March 2016.
1483:Pillet, Nicolas.
1359:
1358:
501:staged combustion
366:staged combustion
274:
273:
268:UR-500 and Proton
45:Country of origin
16:(Redirected from
3596:
3247:
3246:
3083:RD-263, 268, 273
3014:along other LREs
2876:
2736:RD-191, 151, 181
2600:
2258:
2249:
2203:
2196:
2189:
2180:
2146:
2145:
2143:
2142:
2130:
2124:
2123:
2112:
2106:
2105:
2104:on 15 June 2015.
2094:
2088:
2087:
2076:
2070:
2069:
2067:
2066:
2057:. Archived from
2047:
2041:
2040:
2038:
2037:
2028:. Archived from
2018:
2012:
2011:
2009:
2008:
1999:. Archived from
1989:
1983:
1982:
1980:
1979:
1970:. Archived from
1960:
1954:
1953:
1951:
1950:
1941:. Archived from
1931:
1925:
1924:
1922:
1921:
1912:. Archived from
1902:
1896:
1895:
1893:
1892:
1883:. Archived from
1873:
1867:
1866:
1864:
1863:
1858:on June 25, 2002
1854:. Archived from
1844:
1838:
1837:
1835:
1834:
1829:on June 25, 2002
1825:. Archived from
1815:
1806:
1805:
1803:
1802:
1793:. Archived from
1783:
1774:
1773:
1771:
1770:
1765:on June 25, 2002
1761:. Archived from
1751:
1742:
1741:
1730:
1711:
1710:
1708:
1707:
1692:
1686:
1685:
1683:
1682:
1667:
1661:
1660:
1658:
1657:
1642:
1636:
1635:
1633:
1632:
1617:
1606:
1605:
1603:
1602:
1593:. Archived from
1583:
1574:
1573:
1571:
1570:
1555:
1546:
1545:
1534:
1528:
1527:
1525:
1524:
1514:"RD-0212 engine"
1509:
1496:
1495:
1493:
1492:
1480:
1474:
1473:
1462:
992:Thrust (Vacuum)
775:
211:Specific impulse
99:
37:
30:
21:
3604:
3603:
3599:
3598:
3597:
3595:
3594:
3593:
3559:
3558:
3557:
3552:
3534:
3255:
3248:
3244:
3235:
3173:
3063:RD-0255 to 0257
3058:RD-0243 to 0245
2920:
2909:
2905:
2899:
2887:
2863:
2604:
2595:
2585:
2449:
2443:
2437:
2268:
2262:
2243:
2236:
2223:
2221:launch vehicles
2207:
2158:KbKhA Home Page
2154:
2149:
2140:
2138:
2132:
2131:
2127:
2122:on 27 May 2011.
2114:
2113:
2109:
2096:
2095:
2091:
2078:
2077:
2073:
2064:
2062:
2061:on June 2, 2002
2049:
2048:
2044:
2035:
2033:
2020:
2019:
2015:
2006:
2004:
1991:
1990:
1986:
1977:
1975:
1962:
1961:
1957:
1948:
1946:
1945:on May 25, 2002
1933:
1932:
1928:
1919:
1917:
1904:
1903:
1899:
1890:
1888:
1875:
1874:
1870:
1861:
1859:
1846:
1845:
1841:
1832:
1830:
1817:
1816:
1809:
1800:
1798:
1785:
1784:
1777:
1768:
1766:
1753:
1752:
1745:
1732:
1731:
1714:
1705:
1703:
1694:
1693:
1689:
1680:
1678:
1669:
1668:
1664:
1655:
1653:
1644:
1643:
1639:
1630:
1628:
1619:
1618:
1609:
1600:
1598:
1585:
1584:
1577:
1568:
1566:
1557:
1556:
1549:
1544:on 30 May 2015.
1536:
1535:
1531:
1522:
1520:
1511:
1510:
1499:
1490:
1488:
1482:
1481:
1477:
1464:
1463:
1432:
1428:
1364:
1265:
1258:
1251:
1244:
1237:
1230:
1223:
1216:
1073:Isp(Sea Level)
986:
978:
970:
962:
954:
949:
945:
940:
917:
913:
860:
843:
721:
591:
497:
456:Proton-K (8K82)
452:Soviet moonshot
359:S. A. Kosberg's
341:
301:
297:
145:
141:
40:
23:
22:
15:
12:
11:
5:
3602:
3600:
3592:
3591:
3586:
3581:
3576:
3571:
3561:
3560:
3554:
3553:
3551:
3550:
3543:
3539:
3536:
3535:
3533:
3532:
3531:
3530:
3525:
3520:
3515:
3510:
3505:
3500:
3495:
3490:
3485:
3480:
3475:
3470:
3465:
3459:United States
3457:
3456:
3455:
3450:
3445:
3440:
3435:
3430:
3425:
3417:
3416:
3415:
3410:
3402:
3401:
3400:
3395:
3387:
3386:
3385:
3380:
3375:
3370:
3365:
3357:
3356:
3355:
3350:
3345:
3340:
3335:
3330:
3325:
3320:
3315:
3310:
3305:
3300:
3292:
3291:
3290:
3287:
3284:
3279:
3274:
3269:
3260:
3258:
3250:
3249:
3242:
3240:
3237:
3236:
3234:
3233:
3232:
3231:
3225:
3219:
3213:United States
3211:
3210:
3209:
3201:
3200:
3199:
3194:
3185:
3183:
3179:
3178:
3175:
3174:
3172:
3171:
3170:
3169:
3163:
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2152:External links
2150:
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2086:on 5 May 2014.
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2013:
1984:
1955:
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1887:on May 5, 2002
1868:
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1807:
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1695:Zak, Anatoly.
1687:
1670:Zak, Anatoly.
1662:
1645:Zak, Anatoly.
1637:
1620:Zak, Anatoly.
1607:
1597:on May 2, 2002
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1558:Zak, Anatoly.
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1512:Zak, Anatoly.
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1386:vernier engine
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370:M. V. Melnikov
350:started their
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3008:North Korea
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2367:
2310:
2303:
2214:solid motors
2172:
2164:
2139:. Retrieved
2128:
2120:the original
2110:
2102:the original
2092:
2084:the original
2074:
2063:. Retrieved
2059:the original
2054:
2045:
2034:. Retrieved
2030:the original
2025:
2016:
2005:. Retrieved
2001:the original
1996:
1987:
1976:. Retrieved
1972:the original
1967:
1958:
1947:. Retrieved
1943:the original
1938:
1929:
1918:. Retrieved
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1521:. Retrieved
1517:
1489:. Retrieved
1478:
1470:the original
1389:
1384:- Companion
1375:
1370:- Companion
1300:Last Launch
1266:Third Stage
1259:Second Stage
1252:Second Stage
1245:Second Stage
1238:Second Stage
1231:Second Stage
899:Engine Type
870:Development
754:
737:
727:
722:
707:
699:
693:
689:
681:
675:
671:
663:
657:
649:
643:
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572:
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546:
531:
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484:
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408:
400:
396:
392:
388:
384:
382:
342:
328:
324:
285:
277:
275:
270:second stage
78:Manufacturer
59:First flight
3545:Engines in
3192:RD-109, 119
3130:RD-864, 869
3115:RD-854, 861
3078:RD-253, 275
2726:RD-170, 171
1353:References
1295:1967-03-10
1224:First Stage
1217:First Stage
1182:Dry Weight
514:around the
339:Development
186:Performance
109:Predecessor
96:Associated
91:Upper Stage
88:Application
3563:Categories
2932:YF-1, 2, 3
2880:Hypergolic
2852:Rutherford
2571:Prometheus
2533:Archimedes
2173:(Archived)
2165:(Archived)
2141:2015-06-08
2065:2015-06-08
2036:2015-06-08
2007:2015-06-08
1978:2015-06-08
1949:2015-06-08
1920:2015-06-08
1891:2015-06-08
1862:2015-06-08
1833:2015-06-08
1801:2015-06-08
1769:2015-06-08
1706:2015-06-08
1681:2015-06-08
1656:2015-06-08
1631:2015-06-08
1601:2015-06-08
1569:2015-06-08
1523:2015-06-08
1491:2015-06-08
1426:References
1315:1966-07-06
1312:1966-07-06
1309:1964-10-20
1306:1964-10-20
1303:1964-10-20
1292:1967-03-10
1289:1967-03-10
1286:1965-07-16
1283:1965-07-16
1280:1963-11-06
1277:1963-11-06
1274:1963-11-06
1096:Burn Time
894:1962-1967
428:heavy ICBM
345:Chelomey's
229:Dimensions
134:Propellant
62:1967-03-10
3473:Castor 30
3353:Zefiro 40
3348:Zefiro 23
3289:SpaB-140C
2686:NK-33, 44
2596:cryogenic
2442:Methalox
2261:Hydrolox
2253:Cryogenic
2051:"RD-0212"
2022:"RD-0205"
1993:"RD-0202"
1964:"RD-0213"
1935:"RD-0211"
1906:"RD-0210"
1877:"RD-0209"
1848:"RD-0208"
1819:"RD-0206"
1787:"RD-0204"
1755:"RD-0203"
891:1962-1967
888:1962-1967
885:1962-1966
882:1962-1966
879:1961-1964
876:1961-1964
873:1961-1964
536:probe to
317:RD-0203/4
221:Burn time
3488:Orbus-21
3343:Zefiro 9
3106:Ukraine
2884:Aerozine
2872:Storable
2764:Ukraine
2706:RD-0110R
2603:Kerolox
1587:"UR-200"
1362:See also
987:(Fixed)
802:RD-0213
799:RD-0211
796:RD-0210
793:RD-0209
790:RD-0208
787:RD-0206
784:RD-0204
781:RD-0203
589:Versions
549:Venera 9
542:Venera 9
527:Salyut 1
391:and one
292:burning
250:Dry mass
242:Diameter
213:, vacuum
201:pressure
199:Chamber
67:Designer
3547:italics
3508:Star 48
3503:Star 37
3483:Orbus-6
3404:Israel
3338:Waxwing
3294:Europe
3286:SpaB-65
3188:Russia
3053:RD-0237
3048:RD-0236
3019:Russia
2998:Israel
2958:Europe
2802:Kestrel
2748:S1.5400
2711:RD-0124
2677:Russia
2670:SCE-200
2566:Europe
2559:RD-0169
2554:Russia
2480:Longyun
2473:Lingyun
2391:RD-0146
2385:RD-0120
2376:Russia
2333:Vulcain
2319:Europe
2242:Liquid
2218:orbital
1390:RD-0213
1388:of the
1382:RD-0214
1376:RD-0207
1374:of the
1368:RD-0207
1339:Retired
1336:Retired
1333:Retired
1330:Retired
1327:Retired
1324:Status
1125:Length
1068:326.5s
950:(Fixed)
941:(Fixed)
936:Nozzle
863:RD-0214
859:RD-0212
846:RD-0207
842:RD-0205
839:RD-0202
778:Engine
763:RD-0214
755:RD-0212
746:RD-0207
738:RD-0205
728:RD-0202
719:Modules
706:Index:
700:RD-0213
688:Index:
682:RD-0211
670:Index:
664:RD-0210
656:Index:
650:RD-0209
642:Index:
636:RD-0208
624:Index:
618:RD-0206
612:RD-0204
604:Index:
598:RD-0203
579:Russian
505:S1.5400
495:History
489:RD-0214
487:and an
485:RD-0213
481:RD-0212
472:RD-0211
468:RD-0210
460:Korolev
444:RD-0209
440:RD-0208
417:RD-0207
409:RD-0207
401:RD-0206
397:RD-0205
393:RD-0204
389:RD-0203
385:RD-0202
378:S1.5400
362:OKB-154
329:RD-0212
325:RD-0213
286:RD-0211
278:RD-0210
258:Used in
178:Chamber
113:RD-0208
71:OKB-154
18:RD-0203
3463:AJ-60A
3428:KM-V2b
3419:Japan
3393:Salman
3359:India
3333:Topaze
3298:Mage 1
3263:China
3254:Solid
3161:TR-201
3125:RD-856
3120:RD-855
3110:RD-843
3100:S5.98M
3089:RD-270
2983:India
2977:Viking
2967:Astris
2962:Aestus
2952:YF-50D
2928:China
2837:RS-27A
2827:Merlin
2817:LR-105
2781:RD-810
2774:RD-801
2758:TEPREL
2754:Spain
2742:RD-193
2731:RD-180
2721:RD-120
2665:India
2658:Welkin
2651:YF-130
2645:YF-115
2640:YF-102
2635:YF-100
2619:China
2547:Aeon R
2540:Aeon 1
2527:Raptor
2511:YF-215
2504:YF-209
2497:TQ-15A
2461:China
2354:Japan
2343:CE-7.5
2339:India
2294:YF-75D
2280:China
1402:UR-200
1396:Proton
1263:Proton
1256:Proton
1249:Proton
1242:UR-500
1235:UR-500
1228:UR-200
1221:UR-200
1214:UR-200
1153:Width
1065:326.5s
1062:326.5s
908:using
903:Liquid
861:(with
844:(with
828:8D412K
825:8D411K
694:RD-468
690:8D412K
676:RD-465
672:8D411K
575:Zvezda
557:Mars 2
534:Mars 2
512:Zond 5
407:, the
352:UR-200
348:OKB-52
333:Proton
321:Proton
307:in an
288:, are
264:UR-200
234:Length
216:326.5s
119:Status
103:Proton
53:Russia
39:Mockup
3528:X-254
3523:X-248
3513:UA120
3493:Orion
3468:Algol
3453:SRB-A
3448:M-34c
3423:KM-V1
3413:RSA-3
3389:Iran
3282:FG-47
3277:FG-46
3272:FG-36
3267:FG-02
3228:XLR81
3222:RS-88
3217:Curie
3207:Gamma
3182:Other
3166:XLR81
3155:RS-88
3150:LR-91
3145:LR-87
3095:S5.92
3023:17D61
2992:Vikas
2972:Vexin
2947:YF-40
2942:YF-23
2915:, or
2895:, or
2889:UH 25
2857:XLR50
2842:RS-56
2832:RS-27
2812:LR-89
2807:LR-79
2691:RD-58
2681:NK-15
2629:TH-12
2623:TH-11
2594:Semi-
2491:TQ-12
2486:TQ-11
2466:BF-20
2431:RS-68
2426:RS-25
2403:BE-3U
2348:CE-20
2328:Vinci
2312:YF-90
2305:YF-79
2299:YF-77
2289:YF-75
2284:YF-73
1408:KBKhA
1120:250s
979:with
971:with
963:with
955:with
831:8D48
822:8D412
819:8D411
658:8D412
644:8D411
564:Zarya
553:Venus
518:on a
374:OKB-1
343:When
163:Cycle
3518:SRMU
3443:M-34
3438:M-24
3433:M-14
3408:LK-1
3398:Rafe
3383:S200
3378:S139
3328:P230
3323:P120
3256:fuel
3140:AJ10
3002:LK-4
2897:UDMH
2847:S-3D
2768:RD-8
2607:RP-1
2578:M-10
2522:BE-4
2421:RL10
2410:BE-7
2369:LE-9
2363:LE-7
2358:LE-5
2323:HM7B
2244:fuel
2216:for
2212:and
1210:Use
1117:220s
1114:220s
1111:150s
1108:150s
1105:150s
1102:136s
1099:136s
1079:278s
1076:278s
1059:326s
1056:326s
1053:326s
1050:311s
1047:311s
921:UDMH
816:8D47
813:8D44
810:8D44
807:AKA
759:GRAU
742:GRAU
732:GRAU
708:8D48
704:GRAU
686:GRAU
668:GRAU
654:GRAU
640:GRAU
626:8D47
622:GRAU
606:8D44
602:GRAU
538:Mars
516:Moon
470:and
421:R-36
355:ICBM
305:UDMH
303:and
282:GRAU
276:The
266:and
224:220s
149:UDMH
49:USSR
3478:GEM
3373:S12
3318:P80
3313:PAP
3308:P-6
3303:P-4
3203:UK
2987:PS4
2917:HNO
2913:MON
2893:MMH
2797:H-1
2792:F-1
2611:LOX
2453:LOX
2416:J-2
2272:LOX
981:TVC
973:TVC
965:TVC
957:TVC
712:TVC
630:TVC
568:ISS
551:to
464:N-1
462:'s
372:of
313:TVC
158:2.6
3565::
3368:S9
3363:S7
2911:,
2900:/
2891:,
2886:,
2609:/
2451:/
2446:CH
2270:/
2265:LH
2053:.
2024:.
1995:.
1966:.
1937:.
1908:.
1879:.
1850:.
1821:.
1810:^
1789:.
1778:^
1757:.
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1715:^
1699:.
1674:.
1649:.
1624:.
1610:^
1589:.
1578:^
1562:.
1550:^
1516:.
1500:^
1433:^
865:)
585:.
570:.
147:/
98:LV
3230:*
3224:*
3168:*
3157:*
2922:)
2919:3
2908:4
2906:O
2904:2
2902:N
2882:(
2613:)
2605:(
2455:)
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2444:(
2274:)
2267:2
2263:(
2202:e
2195:t
2188:v
2144:.
2068:.
2039:.
2010:.
1981:.
1952:.
1923:.
1894:.
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1836:.
1804:.
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1604:.
1572:.
1526:.
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1378:.
919:/
916:4
914:O
912:2
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702:(
684:(
666:(
652:(
638:(
620:(
600:(
442:/
300:4
298:O
296:2
294:N
280:(
181:1
144:4
142:O
140:2
138:N
51:/
20:)
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