40:
2134:
1811:
380:, was considered more fitting and a less risky choice than Reaction Motors next project. Thus, on October 1, 1955 Martin purchase order 55-3516-CP was signed with General Electric for the X-405 engine for furnishing a self-contained unit which was to include the thrust structure, gimbal ring, engine components, and engine starting equipment.
24:
2198:
2203:
1948:
618:
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1943:
2179:
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The Martin
Company - Engineering Report No. 11022: The Vanguard Satellite Launching Vehicle - An Engineering Summary (April 1960) p. 40-51
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284:
107:
744:
23:
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1045:
1038:
898:
752:
541:
McLaughlin Green, Constance; Lomask, Milton (1970). "Chapter 4 — Getting the Launch
Program Started".
478:
McLaughlin Green, Constance; Lomask, Milton (1970). "Chapter 5 — Battle Over
Vehicle Specifications".
358:
1903:
1772:
1542:
1532:
1223:
1205:
304:
28:
Vanguard rocket engines: rear, GE's first-stage engine; foreground, Aerojet
General's second-stage engine.
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346:. Also, the exhaust gases of the turbine were ducted to dual auxiliary nozzles that acted as
2013:
1993:
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627:
373:
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300:
210:
199:
63:
1412:
830:
391:), used Viking first stages, twelve X-405 were built and eleven flew on Vanguard rockets.
366:
362:
339:
281:
569:"Hydrogen Peroxide - Propulsion & Power History: US - General Electric (1944 - 1966)"
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436:
Bille, Matt; Lishock, Erika (2004). "5 — The Trials of
Project Vanguard".
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361:
got the contract as prime contractor. Given the required thrust levels, the
320:
1978:
1973:
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189:
2108:* Different versions of the engine use different propellant combinations
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rocket was selected as the first orbital launch vehicle for the US,
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Winter, Frank H. (1990). "3 — Rockets Enter the Space Age".
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2008:
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The First Space Race: Launching the World's First
Satellites
319:
experience, the turbine was driven by steam generated by
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376:proposal, based on the experience gained in the
2173:
760:
612:
8:
2199:Rocket engines using the gas-generator cycle
372:) was deemed insufficient, and instead, the
16:
2180:
2166:
1441:
1165:
823:
814:
767:
753:
745:
619:
605:
597:
22:
2204:Rocket engines using kerosene propellant
315:. As was common to engines based on the
399:
383:While the first two Vanguard flight, (
350:to enable roll control of the rocket.
79:
15:
7:
2130:
2128:
798:Comparison of orbital rocket engines
2152:. You can help Knowledge (XXG) by
544:Vanguard: A History (NASA SP-4202)
481:Vanguard: A History (NASA SP-4202)
14:
237:1.14 m (3 ft 9 in)
2132:
1809:
38:
334:and the combustion chamber was
444:Texas A&M University Press
1:
1594:RD-0202 to 0206, 0208 to 0213
179:123.8 kN (27,800 lb
167:134.8 kN (30,300 lb
94:General Electric Hermes A-3B
303:. It was used to power the
216:248 s (2.43 km/s)
194:4.2 MPa (610 psi)
2225:
2127:
205:270 s (2.6 km/s)
2104:
1807:
793:
412:Encyclopedia Astronautica
254:
245:191 kg (421 lb)
21:
515:Harvard University Press
285:liquid-propellant rocket
1639:RD-250 to 252, 261, 262
338:cooled. The engine was
2148:-related article is a
2115:are under development
1503:YF-20, 21, 22, 24, 25
1282:RD-107, 108, 117, 118
571:. Whiskey Yankee LLC
1604:RD-0216, 0217, 0235
1267:RD-0107, 0108, 0110
299:cycle developed by
18:
509:Rockets Into Space
108:Liquid-fuel engine
2209:Outer space stubs
2161:
2160:
2122:
2121:
2064:Space Shuttle SRB
1805:
1804:
1743:
1742:
1433:
1432:
1155:
1154:
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323:decomposition of
274:
273:
176:Thrust, sea-level
34:Country of origin
2216:
2182:
2175:
2168:
2136:
2129:
1813:
1812:
1649:RD-263, 268, 273
1580:along other LREs
1442:
1302:RD-191, 151, 181
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628:Project Vanguard
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414:. Archived from
404:
374:General Electric
365:propulsion (the
344:thrust vectoring
313:Vanguard project
309:Vanguard rockets
301:General Electric
211:Specific impulse
200:Specific impulse
81:
64:General Electric
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1629:RD-0255 to 0257
1624:RD-0243 to 0245
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586:Further reading
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287:engine burning
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776:Rocket engines
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446:. p. 94.
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378:Hermes program
359:Martin Company
336:regeneratively
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1578:Paektusan LRE
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1574:North Korea
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780:solid motors
573:. Retrieved
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552:. Retrieved
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522:. Retrieved
508:
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489:. Retrieved
480:
457:. Retrieved
438:
431:
420:. Retrieved
416:the original
402:
382:
352:
277:
275:
151:Nozzle ratio
60:Manufacturer
2146:spaceflight
2111:Engines in
1758:RD-109, 119
1696:RD-864, 869
1681:RD-854, 861
1644:RD-253, 275
1292:RD-170, 171
305:first stage
258:first stage
224:145 seconds
213:, sea-level
159:Performance
91:Predecessor
78:Associated
73:First stage
70:Application
2193:Categories
1498:YF-1, 2, 3
1446:Hypergolic
1418:Rutherford
1137:Prometheus
1099:Archimedes
734:Vanguard 3
729:Vanguard 2
724:Vanguard 1
717:Satellites
575:2015-06-24
554:2015-06-24
524:2015-06-24
517:. p.
491:2015-06-24
459:2015-06-24
422:2015-06-24
395:References
342:to supply
268:References
263:References
229:Dimensions
114:Propellant
2039:Castor 30
1919:Zefiro 40
1914:Zefiro 23
1855:SpaB-140C
1252:NK-33, 44
1162:cryogenic
1008:Methalox
827:Hydrolox
819:Cryogenic
353:When the
321:catalytic
221:Burn time
2054:Orbus-21
1909:Zefiro 9
1672:Ukraine
1450:Aerozine
1438:Storable
1330:Ukraine
1272:RD-0110R
1169:Kerolox
635:Launches
355:Vanguard
348:verniers
340:gimbaled
282:pump-fed
256:Vanguard
242:Dry mass
234:Diameter
202:, vacuum
190:pressure
188:Chamber
85:Vanguard
2113:italics
2074:Star 48
2069:Star 37
2049:Orbus-6
1970:Israel
1904:Waxwing
1860:Europe
1852:SpaB-65
1754:Russia
1619:RD-0237
1614:RD-0236
1585:Russia
1564:Israel
1524:Europe
1368:Kestrel
1314:S1.5400
1277:RD-0124
1243:Russia
1236:SCE-200
1132:Europe
1125:RD-0169
1120:Russia
1046:Longyun
1039:Lingyun
957:RD-0146
951:RD-0120
942:Russia
899:Vulcain
885:Europe
808:Liquid
784:orbital
709:/TV4-BU
408:"X-405"
311:on the
307:of the
250:Used in
143:Chamber
102:Retired
2029:AJ-60A
1994:KM-V2b
1985:Japan
1959:Salman
1925:India
1899:Topaze
1864:Mage 1
1829:China
1820:Solid
1727:TR-201
1691:RD-856
1686:RD-855
1676:RD-843
1666:S5.98M
1655:RD-270
1549:India
1543:Viking
1533:Astris
1528:Aestus
1518:YF-50D
1494:China
1403:RS-27A
1393:Merlin
1383:LR-105
1347:RD-810
1340:RD-801
1324:TEPREL
1320:Spain
1308:RD-193
1297:RD-180
1287:RD-120
1231:India
1224:Welkin
1217:YF-130
1211:YF-115
1206:YF-102
1201:YF-100
1185:China
1113:Aeon R
1106:Aeon 1
1093:Raptor
1077:YF-215
1070:YF-209
1063:TQ-15A
1027:China
920:Japan
909:CE-7.5
905:India
860:YF-75D
846:China
662:TV-3BU
450:
363:Viking
280:was a
99:Status
43:
2144:- or
2142:space
2140:This
2094:X-254
2089:X-248
2079:UA120
2059:Orion
2034:Algol
2019:SRB-A
2014:M-34c
1989:KM-V1
1979:RSA-3
1955:Iran
1848:FG-47
1843:FG-46
1838:FG-36
1833:FG-02
1794:XLR81
1788:RS-88
1783:Curie
1773:Gamma
1748:Other
1732:XLR81
1721:RS-88
1716:LR-91
1711:LR-87
1661:S5.92
1589:17D61
1558:Vikas
1538:Vexin
1513:YF-40
1508:YF-23
1481:, or
1461:, or
1455:UH 25
1423:XLR50
1408:RS-56
1398:RS-27
1378:LR-89
1373:LR-79
1257:RD-58
1247:NK-15
1195:TH-12
1189:TH-11
1160:Semi-
1057:TQ-12
1052:TQ-11
1032:BF-20
997:RS-68
992:RS-25
969:BE-3U
914:CE-20
894:Vinci
878:YF-90
871:YF-79
865:YF-77
855:YF-75
850:YF-73
707:SLV-7
702:SLV-6
697:SLV-5
692:SLV-4
687:SLV-3
682:SLV-2
677:SLV-1
370:XLR10
295:in a
278:XLR50
128:Cycle
17:XLR50
2150:stub
2084:SRMU
2009:M-34
2004:M-24
1999:M-14
1974:LK-1
1964:Rafe
1949:S200
1944:S139
1894:P230
1889:P120
1822:fuel
1706:AJ10
1568:LK-4
1463:UDMH
1413:S-3D
1334:RD-8
1173:RP-1
1144:M-10
1088:BE-4
987:RL10
976:BE-7
935:LE-9
929:LE-7
924:LE-5
889:HM7B
810:fuel
782:for
778:and
672:TV-5
667:TV-4
657:TV-3
652:TV-2
647:TV-1
642:TV-0
549:NASA
486:NASA
448:ISBN
389:TV-1
387:and
385:TV-0
291:and
289:RP-1
276:The
122:RP-1
55:1957
52:Date
2044:GEM
1939:S12
1884:P80
1879:PAP
1874:P-6
1869:P-4
1769:UK
1553:PS4
1483:HNO
1479:MON
1459:MMH
1363:H-1
1358:F-1
1177:LOX
1019:LOX
982:J-2
838:LOX
317:V-2
293:LOX
154:5.5
118:LOX
2195::
1934:S9
1929:S7
1477:,
1466:/
1457:,
1452:,
1175:/
1017:/
1012:CH
836:/
831:LH
547:.
533:^
519:71
513:.
484:.
468:^
442:.
410:.
120:/
80:LV
2181:e
2174:t
2167:v
2156:.
1796:*
1790:*
1734:*
1723:*
1488:)
1485:3
1474:4
1472:O
1470:2
1468:N
1448:(
1179:)
1171:(
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557:.
527:.
494:.
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329:O
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325:H
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181:f
171:)
169:f
146:1
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