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Aviation History
1962
1962 - 1028.PDF
1026 FLIGHT International, 28 June 1962 TABLE3: TURBOPROPS Designat Manufacturer Allison 250 501-D13 BS Gnome P.1200 Proteus 765 CP & WA PT6A-6 GE Lycoming LTC4G-3 Napier Eland 504 R-R Dart 3 Dart 6 Dart 7/2 Dart 10/1 Dart 12 Tyne 11 Tyne 12 Tyne 20 Tyne 22 Tyne 32 Rover TP/90 Turb. Astazou 2 Bastan 4 Oredon 2 Turmo 3D2 Turmo 3D3 Turmo 6 on Military YT63 — T56-1A T56-10W — Mk255 YT74 T64-8 T53-7 T55 — — — — — — — Mk 101 Mk21,22 — — — — — — — — Engine configuration 6a + lc, 2ct, 2pt 14a, 4t 14a, 4t 14a, 4t 10a, 2ct, lpt 12a+lc, 2ct,2pt 3a + lc, let, lpt 14a, 2ct, 2pt 5a + lc, let, lpt 7a + lc, let, 2pt 10a, 3t 2c, 2t 2c, 2t 2c, 3t 2c, 3t 2c, 3t 6a, 9a, It, 3t 6a, 9a, It, 3t 6a, 9a, It, 3t 6a, 9a, It, 3t 6a, 9a, It, 3t lc, It la+lc, 3t la + lc, 3t la+lc, 3t la+lc, 2ct, lpt la + lc, 2ct,2pt 2a + lc, 2ct, 2pt Length (in) 145.2 145.1 145.1 79.3 100.6 62 113 58.4 62.2 95.5 95 98 98 99.49 99.49 108.7 108.7 108.7 35.44 68.4 74.4 60 72 76 Diam. (to) 27 27.5 27.5 17* 40.1 19 24t 23 24.76 36 ' 38 38 38 38 38 43.2 43.2 43.2 19.9 18 22 14.4 34.44 34.44 Weight 0b) 1,750 1,645 — 595 2,900 270 — 540 795 1,820 1,026 1,106 1,227 1,377 1,378 2,275 2,177 2,203 200 271 468* 202 661 661 881 Air flow Ob/sec) 32.5 32.5 — 12.3 46 5 24.5 10.7 — 33.5 20.5 20.5 23.5 27 27 46.5 46.5 46.5 1.88 5.56 9.8 2.5 13 13 Press. 9.25 9.25 — 8.1 7.3 6 12.6 6 —• 7 5.4 5.4 5.6 6.35 6.35 13.5 13.5 13.5 2.8 6 5.5 6 5.5 5.5 Maximum power s.b.p.; c.h.p.; r.p.m. 250; 3,460; 3,740; 13,820 3,460; 3,740; 13,820 ; 4,585; 13,820 1,150; 1,200; 26,260 3,915;4,445; 11,700 550; 578; 37,500 ; 2,850; 15,590 1,100; 1,150; 26,000 2,445; 2,535; 18,750 3,230; 3,500; 12,500 1,345; 1,480; 14,500 1,535; 1,670; 14,500 1,910; 2,100; 15,000 2,750; 3,030; 15,000 ; 3,245; 15,000 4,850; 5,325; 15,250 5,095; 5,505; 15,250 5,440; 5,855; 15,250 6,625;7,075; 15,250 7,870; 8,400; 15,250 118; 118; 47,000 530; 562; 43,500 917; 986; 33,500 196; 207; 59,000 1,285; 1,335; 22,460§ 1,450; — ; 33,500 1,800; — ; 32,000 Typical cruise power Feet; knots; c.h.p.; s.f.c. 6,000; 200; 206; 0.73 25,000; 360; 1,905; 0.467 — — 0;0; 805:0.728 25,000; 340; 2,675; 0.501 0;0; 495; 0.68 20,000; 370; 1,522; 0.493 — .— 20,000; 261; 1,660; 0.56 20,000; 300; 955; 0.65 20,000; 300; 985; 0.634 20,000; 300; 1,315; 0.573 20,000; 300; 1,615; 0.556 20,000; 300; 1,612; 0.555 25,000; 370; 3,195; 0.384 25,000; 370; 3,220; 0.388 25,000; 320; — — 0; any; 100; 1.36 20,000; 270; 398; 0.492 9,900; 350; 795; 0.58 — 0; 0; 855; 0.737 — TBO (hr) 2,200 — — 2,400 — — — — 800 4,000 3,500 3,000 — .— 2,000 1,000 — — — — — — — Main applications _ Electra C-130A Hercules P3V-1 Britannia 320 — — AO-1 CL-66 V.700 V.700D V.810, AW.650, F.27, 748 Herald, Gulfstream YS-11 HP.124, 748MF Vanguard CL-44, Yukon, Belfast Br.1150, Transall — — Potez 840, Marquis, Porter Sup. Broussard, Spirale Br.941, 942 Spirale III Br.943 * Height 31.55in; t height 46in; tcowled powerplant: § free-turbine speed. TABLE 4: TURBOSHAFTS Designation Manufacturer Military AiResearch 331 Allison 250-C BMW 6012 Boeing 520-6 BS Gnome H.1200 Coupled Gnome H.1200 Nimbus 750 CP & WA PT6B-9 Continental 217-5A DB PTL6 Fiat 4301.000 GE CT58-100-1 Lycoming LTC1B-1 LTC1 LTC4 Napier Gazelle P & WA JFTD12 Turb. Artouste 2C Artouste 3B Turmo 3C3 T63-5 YT60 Mk 101 MkllO Mk 100 YT74 T72-2 T58-8B T64-2 T64-6 T53-1A T53-9 T55-5 Mkl62 Engine configuration 2c,3t 6a + lc, 2ct, 2pt lc, It 1c, let, lpt 10a, 2ct, lpt 2 X Gnome 2a+lc, 2ct, lpt 3a + lc, let, lpt la+lc, 2ct, lpt 4a + lc, 2ct, lpt lc, let, lpt 10a, 2ct, lpt 10a, 2ct, lpt 14a, 2ct, 2pt 14a, 2ct, 2pt Sa+lc, let, lpt 5a+lc, let, lpt 7a + lc, lct,2pt 11a, 2ct. lpt 9a, 2ct, 2pt lc, 2t la + lc, 3t la + lc, 2ct,2pt Length (in) 40.5 38.5 24.5 57.3 54.8 78 61.6 59 42.48 70 59 55 55 91 83 47.61 47.61 45.46 70* 56.4 57.6 66.5 Diam. (in) Weight (lb) 18.54 15.8 15 25.5 17 41 20.1 19 19.38 20.3 22.4 16 16 25 24 23 23 24.76 33.5 21.9 20.4 20.4 25.8 Air flow (lb/sec) 199 147 100 325 328 1,043 390 245 210 440 386 304 295 864 713 484 485 570 920 870 253 287 414 4.39 5.3 12.3 24.6 11 5 10.4 12.4 12.4 24.5 24.5 10.7 10.7 16.5 9.5 13 Press, ratio 6.25 8.1 8.1 6.5 6 4 8.3 8.3 12.6 12.6 6 6 <u 6.5 3.88 5.2 5.5 Max. power s.h.p.; r.p.m.; minutes time 500; 39,000; 250; 48,750; 89; 45,000; 550; 1,250; 26,750; 2| 1,000; 35,300; 5 550; 37,500; 500; 42,500; 5 1,050; 18,600; 690; 25,000 1,050; 26,260; 5 1,250; 26,260; 5 2,810; 13,600; 10 2,850; 13,600; 860; 25,240; 1,100:26,000; 2,200; 14,550; 1,575; 19,900; 4,050; 500; 34,000; cont 550; 34,000; cont 1,500;33,500; Output r.p.m. 6,000 6,020 3-8,000 6,000 19,500 2,915 2,150 6,230 5,976 6,000 19,500 19,500 5,200 13,600 6,680 6,610 14,550 2,500 9,000 6,000 6,000 5,700 Rated or lhr power Feet; knots; s.h.p.; s.f.c.; r.p.m. 0;0; 191; 0.77; 46,100 0; 0; 500; 0.67; 10,000; 100; 950; 0.602; 25,920 5,000; 0; 770; 0.705 0;0; 485; 0.69; 6,000; 0; 265; 0.78; 41,000 0; 0; 760; 0.70; 10,000; 0; 785; 0.63; 25,920 20,000; 0; 680; 0.585; 25,920 15,000; 100; 1,720; 0.494; 13,600 15,000; 100; 1,750; 0.485; 13,600 0; 0; 1,330; 0.695; 19,300 0; 0; 3,200; 0; 0; 345; 1.02; 32,000 3,280; 0; 405; 0.81; Main applications LOH helicopters Sailplanes Agustas, W'wind, 107 Wessex 2 and 4 Scout, Wasp, SR.N2 Hiller Ten99, Piasecki 107, S-61L. S-62 HRB-1, HU2K, HSS-2 XC-142 HU-1, H^»3B HU-1D HC-1B Wessex 31 S-64 Alouette 2 Alouette 3 Super Frelon 1 Along engine axis; engine is installed diagonally. TABLE 51 PISTON ENGINES Designation Agusta GA.40 GA.70V A.140V Alvis Leonides 531 Ardem 4C02 Continental A65 O200A O300A IO470D Franklin 2A-110 4A-225 6AGS-335 Lycoming IO360 TV0435-A1A GO480-B1A6 IO540 IGSO540-B1A VO540-C1A M-332 M-337 Meteor Alfa 4 Alfa 5 Potez 4D-34 4E-20 6E-00 Configuration 02 04, vert 04, vert R9,g,s 04 04 04 06 06, inj 02 04 06, inj, g, turb 04, inj 06, vert, turb 06.B 06, inj 06, inj, g, s 06, vert I4L I6L, s (opt.) R8 R8 I4L.S 04 06 Dimensions (inches) Length 24.1 18.5 22.83 54.4 — 30.4 28.53 39.75 43.31 23.7 30.5 41 32.81 34.73 39.84 38.62 48.5 34.73 43.4 55.5 45.27 34.25 46.8 30.7 37.3 Width 30.9 21.26 31.49 41.5 — 31.5 31.56 31.5 33.56 30.7 31.5 31.6 33.37 33,58 33.12 34.25 34.25 34.7 16.7 18.4 23.4 23.4 20.5 30.1 30.6 Height 17.71 18.5 27.17 41.5 — 20.3 23.18 23.25 19.75 22.7 25.1 21.25 22.47 36.51 28.02 19.6 20.29 24.58 23.9 24.7 23.4 23.4 27.6 23.9 22.7 Weight 0b) 123.46 176.4 255.8 860 133 170 190 268 426 130 228 410 291 468 432 437 532 439 225 313 320 268 408 207 275 Bore (to) 3.937 3.622 4.51 4.8 3.031 3.875 4.0625 4.0625 5 4.5 4.5 4.5 5.125 4.875 5.125 5.125 5.125 5.125 4.13 4.13 4.133 4.133 4.921 4.33 4.33 Stroke (to) 3.74 3.4 3.49 4.8 2.52 3.625 3.875 3.875 4 3.5 3.5 3.5 4.375 3.875 3.875 4.375 4.375 4.375 4.53 4.53 3.071 3.071 4.724 3.543 3.543 Cap acity (cuin) 91.1 140.3 222.93 783 72.62 171 201 301 471 112 225 335 360 435 480 540 540 540 242.78 364.25 329.52 329.52 357 209 313 Fuel grade 80/87 80/87 91 100/130 80 73 80/87 80/87 100/115 100/130 80/87 100/130 91/96 100/130 80/87 100/130 100/130 100/130 72 72 — — 100/130 80/87 100/130 Maximum power h.p.; r.p.m. 41; 2,700 82; 3,300 139; 3,200 650; 3,200 30.7;3,000 65; 2,300 100; 2,750 145;2,700 260; 2,625 60; 3,000 125; 2,800 260; 3.200* 180; 2,700 260; 3,200t 270; 3,400 290; 2,575 380; 3,400 305; 3,200 140; 2,700 210; 2,750 220; 2,800 320; 4,000 260; 2,550 105; 2,750 153; 2,700 Typical cruise power Ft; h.p; r.p.m.; gal/hr 0; 20; 2,000; 1.45 0; 64; 3,000; 4.65 5,000; 107; 3,000; 10,250; 360; 2,600; 25 — 0; 43; 2,000; 3.1 0; 65; 2,500; 0; 103; 2,400; 5,000; 188; 2,300; 0; 0; 60; 3,000; 0; 0; 125; 2,800; 15,000; 0; 230; 3,200; 7,500; 135; 2,450; — 6,000; 195; 2,750; 6,000:220:2,350: 13,000; 270; 2,750; 9,500; 240; 3,200; 1,000; 95; 2,400; 5.61 5,000; 140; 2,400; — — 0; 200; 2,400; 0; 75; 2,450; 0; 107; 2,400; Main applications Agusta A 103B Agusta A104 Scottish Aviation Twin Pioneer 3 Rollason Turbulent — Cessna 150, Emeraude Super Rallye, Beagle 117 & 218 Cessna 310 — — — Mousquetaire, Travel Air, Airedale Bell, Agustas Do27 Aero Commander 500B Aero Commander 680F Hillers Aero 145, Meta-Sokol Morava L.200A — Targets and drones Nord 3202,3400 1051 Ambassadeur """ • At up to 10,000ft; t At up to 13,000ft.
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