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de Havilland Spectre

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In 1952 static testing commenced with the Spectre DSpe.l. The aircraft industry had no precedent for an engine which would gain in thrust with altitude and the required maximum thrust was estimated at between 2,000 lbf (8.9 kN) and 15,000 lbf (67 kN) thrust. The design was based
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on a variable thrust which could be throttled from 8,000 lbf (36 kN) to 2,000 lbf (8.9 kN). Design philosophy was matched to the mixed power concept of an aircraft having both a turbojet and rocket engine for maximum operational flexibility.
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Development flying of the SR.53 continued through 39 flights operating to Mach 1.33, and to altitudes at 55,000 ft (17,000 m), as research and construction proceeded on the SR.177, until its cancellation in 1958.
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engine, thus meeting a full mixed-power aircraft concept. In conjunction with the new engine, development had been undertaken with two major ancillaries, a peroxide starter for the gas turbine and a peroxide
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with pump stages both upstream and downstream, gauze catalyst packs, low-loss internal-flow turbine and the use of straight kerosene fuel. The aircraft tanks were to be pressurised to suppress pump
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Primary innovation was as the first to incorporate its turbo pump turbine upstream of its combustion chamber. Described then as low loss. Technological innovation embraced the
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declaring that all future combat would be undertaken by computer-controlled missiles, and that crewed interceptors were now considered obsolete.
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it used the same fuel tanks as the turbojet engine and if run at full power was expected to consume the full load in about seven minutes.
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to utilise a revised design Spectre DSpe.5 engine together with a reheated supersonic capability 14,000 lbf (62 kN) thrust
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in the 1950s. It was one element of the intended mixed power-plant for combination rocket-jet interceptor aircraft of the
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nuclear stand off bomb, with two chambers arranged vertically; a fixed thrust D.Sp.4 above a variable thrust D.Sp.5.
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The Spectre project was cancelled in October 1960, at a reported total cost of £5.75 million.
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In October 1957 a contract was announced for a more advanced version of the aircraft as the
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It went through rig tests commencing in 1953, bench tests from mid-1954, and testing in two
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Barske, U. M. (1960). "Development of Some Unconventional Centrifugal Pumps".
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Development of Dspe.2, constant thrust RDS.15 ATO – "limited quantities".
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The conventional Spectre DSpe.5 had been developed alongside a DSpe.4
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Preserved Spectre engines are on display at the following museums:
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A doubled version of this engine, used for early flight-testing of
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10,000 lbf (44,000 N) thrust version intended for the
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Rocket engines using hot cycle hydrogen peroxide propellant
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After merging of interests in 1959, it was manufactured by
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In the 1127: 938: 924: 476:8,000 lbf (36,000 N) (full power) 819:"British Aero Engines, 1957 : Spectre" 318:stand-off bomb, together with the peroxide 260:Development of Dspe.1 with variable thrust. 1134: 1120: 931: 917: 701: 412: 388: 1142:Aviation rocket engines and rocket motors 665: 322:, from its first flight in October 1959. 122: 1316:Rocket engines using kerosene propellant 659: 397:Spectre rocket engine on display at the 392: 254:Constant thrust version, simpler design. 230:Double Spectre engine on display at the 225: 622:"Cancelled projects: the list up-dated" 38:de Havilland Spectre on display at the 1298: 547: 408:Aircraft engines of the World 1959/60. 1115: 912: 668:Aircraft engines of the World 1959/60 363: 16:1950s British aircraft rocket engine 891:"Aero engines, 1961 : Spectre" 873:"Aero engines, 1959 : Spectre" 13: 867:(2599): 765–766. 14 November 1958. 678: 14: 1332: 849:(2559): 178–179. 7 February 1958. 562:10.1243/PIME_PROC_1960_174_037_02 162:, as formerly researched in the 29: 533:"More About the Super Sprite". 325: 742:(2432): 395. 2 September 1955. 638: 596: 585:. 4 March 1955. Archived from 568: 541: 526: 464: 373:Royal Air Force Museum Cosford 1: 1306:De Havilland aircraft engines 519: 452: 431:56.4 in (1,430 mm) 855:"Development of the Spectre" 831:(2536): 336. 30 August 1957. 634:(3049): 262. 17 August 1967. 399:de Havilland Aircraft Museum 378:De Havilland Aircraft Museum 299:variant, the latter for the 40:de Havilland Aircraft Museum 7: 1192:Armstrong Siddeley Screamer 885:(2617): 392. 20 March 1959. 780:"de Havilland engines 1957" 666:Wilkinson, Paul H. (1959). 485: 448:Hydrogen peroxide/Kerosene 221: 109:de Havilland Engine Company 10: 1337: 1197:Armstrong Siddeley Snarler 748:"At Farnborough Next Week" 232:Rolls-Royce Heritage Trust 1267: 1246: 1230: 1147: 1088: 1062: 1041: 1010: 949: 903:(2732): 79. 20 July 1961. 760:(2432). 2 September 1955. 437:27 in (690 mm) 190:de Havilland Gyron Junior 158:high-speed open-impeller 37: 28: 23: 1285:Rocket assisted take off 1275:List of aircraft engines 788:: 297–298. 8 March 1957. 774:: 450. 9 September 1955. 648:. Skomer. Archived from 606:. Skomer. Archived from 514:List of aircraft engines 423:Liquid-propellant rocket 202:1957 Defence White Paper 1311:Aircraft rocket engines 1280:List of rocket aircraft 1177:Bristol Siddeley BS.605 687:"Britain's New Engines" 413:General characteristics 389:Specifications (D.Sp.5) 284:DSpe.D.1 Double Spectre 1254:Type 4 Mark 1 Model 20 1042:Turboprops/turboshafts 813:: 245. 23 August 1957. 421:fully variable thrust 401: 383:East Midlands Aeropark 238: 123:Design and development 107:that was built by the 1096:Geoffrey de Havilland 550:Proc. Inst. Mech. Eng 396: 229: 1182:de Havilland Spectre 766:"Tomorrow's Engines" 627:Flight International 592:on 15 February 2006. 497:Bristol Siddeley 605 198:auxiliary power unit 168:regenerative cooling 101:de Havilland Spectre 1187:de Havilland Sprite 610:on 2 December 2008. 343:Handley Page Victor 305:Handley-Page Victor 280:Saunders-Roe SR.177 241:Variants included: 117:Saunders-Roe SR.177 1217:Walter HWK 109-509 1212:Dushkin D-1-A-1100 837:"Spectre ATO unit" 695:: 572. 6 May 1955. 491:Comparable engines 402: 364:Engines on display 353:Saunders-Roe SR.53 337:Blue Steel missile 316:Blue Steel missile 239: 127:The Spectre was a 92:Saunders-Roe SR.53 87:Major applications 1293: 1292: 1231:Hybrid propellant 1109: 1108: 160:centrifugal pumps 137:hydrogen peroxide 97: 96: 1328: 1268:Related articles 1247:Solid propellant 1222:Toku-Ro.2 (KR10) 1136: 1129: 1122: 1113: 1112: 933: 926: 919: 910: 909: 904: 886: 868: 850: 832: 814: 800: 799:. 5 August 1957. 789: 775: 761: 743: 725: 724:. 5 August 1955. 712: 696: 672: 671: 663: 657: 656: 654: 646:"Double Spectre" 642: 636: 635: 618: 612: 611: 600: 594: 593: 591: 580: 572: 566: 565: 545: 539: 538: 530: 358:Vickers Type 559 349:only for trials) 248:Initial version. 213:Bristol Siddeley 88: 58: 33: 21: 20: 1336: 1335: 1331: 1330: 1329: 1327: 1326: 1325: 1296: 1295: 1294: 1289: 1263: 1242: 1226: 1202:Napier Scorpion 1143: 1140: 1110: 1105: 1084: 1058: 1037: 1006: 945: 937: 907: 730:"Rocket Motors" 681: 679:Further reading 676: 675: 664: 660: 655:on 5 June 2011. 652: 644: 643: 639: 619: 615: 602: 601: 597: 589: 578: 574: 573: 569: 556:(11): 437–461. 546: 542: 537:. 29 July 1955. 532: 531: 527: 522: 502:Napier Scorpion 488: 467: 455: 415: 391: 366: 328: 224: 131:engine burning 125: 113:Royal Air Force 86: 57:National origin 56: 17: 12: 11: 5: 1334: 1324: 1323: 1318: 1313: 1308: 1291: 1290: 1288: 1287: 1282: 1277: 1271: 1269: 1265: 1264: 1262: 1261: 1256: 1250: 1248: 1244: 1243: 1241: 1240: 1238:RocketMotorTwo 1234: 1232: 1228: 1227: 1225: 1224: 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Kingdom 59: 53: 52: 47: 43: 42: 35: 34: 26: 25: 15: 9: 6: 4: 3: 2: 1333: 1322: 1319: 1317: 1314: 1312: 1309: 1307: 1304: 1303: 1301: 1286: 1283: 1281: 1278: 1276: 1273: 1272: 1270: 1266: 1260: 1257: 1255: 1252: 1251: 1249: 1245: 1239: 1236: 1235: 1233: 1229: 1223: 1220: 1218: 1215: 1213: 1210: 1208: 1207:Dushkin S-155 1205: 1203: 1200: 1198: 1195: 1193: 1190: 1188: 1185: 1183: 1180: 1178: 1175: 1173: 1170: 1168: 1165: 1163: 1160: 1158: 1155: 1154: 1152: 1150: 1146: 1137: 1132: 1130: 1125: 1123: 1118: 1117: 1114: 1102: 1101:Frank Halford 1099: 1097: 1094: 1093: 1091: 1087: 1081: 1078: 1076: 1073: 1071: 1068: 1067: 1065: 1061: 1055: 1052: 1050: 1047: 1046: 1044: 1040: 1034: 1031: 1029: 1026: 1024: 1021: 1019: 1016: 1015: 1013: 1009: 1003: 1000: 998: 995: 993: 990: 988: 985: 983: 980: 978: 975: 973: 970: 968: 965: 963: 960: 958: 955: 954: 952: 948: 944: 941: 934: 929: 927: 922: 920: 915: 914: 911: 902: 898: 897: 892: 888: 884: 880: 879: 874: 870: 866: 862: 861: 856: 852: 848: 844: 843: 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105:rocket engine 102: 93: 90: 85: 84: 80: 77: 76: 73: 70: 68:Manufacturer 67: 66: 63: 60: 55: 54: 51: 50:Rocket engine 48: 45: 44: 41: 36: 32: 27: 22: 19: 1259:Jetex engine 1181: 1079: 1075:Super Sprite 1033:Gyron Junior 992:Gipsy Twelve 967:Gipsy Junior 943:aero engines 940:de Havilland 900: 894: 882: 876: 864: 858: 846: 840: 828: 822: 808: 794: 783: 769: 757: 751: 739: 733: 719: 711:: 838. 1955. 706: 703:"Paris Show" 690: 667: 661: 650:the original 640: 631: 625: 616: 608:the original 598: 587:the original 582: 570: 553: 549: 543: 534: 528: 507: 506: 490: 489: 479: 470: 458: 445: 440: 434: 428: 418: 407: 404: 403: 367: 346: 332:Aerfer Leone 326:Applications 294: 240: 217: 210: 206: 183: 176: 153: 149: 129:bipropellant 126: 100: 98: 72:de Havilland 18: 1149:Liquid fuel 987:Gipsy Queen 977:Gipsy Major 972:Gipsy Minor 793:"Spectre". 718:"Spectre". 465:Performance 441:Dry weight: 301:Avro Vulcan 1300:Categories 997:Gipsy King 520:References 480:Burn time: 453:Components 289:Blue Steel 174:problems. 172:cavitation 78:First run 1089:Designers 1011:Turbojets 982:Gipsy Six 805:"Spectre" 604:"Spectre" 435:Diameter: 405:Data from 308:V bombers 179:Canberras 486:See also 312:Hatfield 222:Variants 193:turbojet 133:kerosene 24:Spectre 1162:XR-4K14 1080:Spectre 1063:Rockets 653:(image) 429:Length: 425:engine 275:DSpe.5A 1157:XR-4A3 1070:Sprite 1023:Goblin 896:Flight 878:Flight 860:Flight 842:Flight 824:Flight 810:Flight 796:Flight 785:Flight 771:Flight 753:Flight 735:Flight 721:Flight 708:Flight 692:Flight 472:Thrust 459:Pumps: 339:(Avro) 269:DSpe.5 263:DSpe.4 257:DSpe.3 251:DSpe.2 245:DSpe.1 186:SR.177 164:Walter 156:Barske 1172:XLR99 1167:XLR11 1049:Gnome 1028:Gyron 1018:Ghost 962:Gipsy 957:Ghost 590:(PDF) 579:(PDF) 446:Fuel: 419:Type: 347:XA930 236:Derby 145:SR.53 103:is a 81:1952 46:Type 1002:Iris 303:and 297:RATO 135:and 99:The 1054:Gem 558:doi 554:174 320:APU 141:lbf 1302:: 901:80 899:. 893:. 883:75 881:. 875:. 865:74 863:. 857:. 847:73 845:. 839:. 829:72 827:. 821:. 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Index


de Havilland Aircraft Museum
Rocket engine
United Kingdom
de Havilland
Saunders-Roe SR.53
rocket engine
de Havilland Engine Company
Royal Air Force
Saunders-Roe SR.177
bipropellant
kerosene
hydrogen peroxide
lbf
SR.53
Barske
centrifugal pumps
Walter
regenerative cooling
cavitation
Canberras
SR.177
de Havilland Gyron Junior
turbojet
auxiliary power unit
1957 Defence White Paper
Bristol Siddeley

Rolls-Royce Heritage Trust
Derby

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