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Aviation History
1919
1919 - 0206.PDF
M FWMtUAJtY IS, IQI0 RECORD OF PERFORMANCES OF BRITISH AEROPLANES. (From information supplied by the U.S. Government.) Type. N Cl X V B a. h E ; i 2 - ii. rt 1 0 • z 3| Engine. Normal b.h.p. and r.p.m. at G.L. ace . 1 £ ? 3 IS j s 8 ti-r •jf v < Speed in m.p.h. and r.p.m. @ 10,000 it. Time in Mins. and Rate of Climb in ft. per minute and r.p.m. @ 10,000 ft. 6,500'- Rate and r.p.m. 15,000' I H Loading Com parative Perform ance. See Note. At 10,000' Weight, lbs. a 2 + 6) • + i Dimenaions. I De Havilland 9 a De Havilland| 9 b De Havilland »* De Havilland 9d S.E. 5 Bristol Fighter Blackburn Kangaroo Sop with Hippo De Haviliand] 9 Sopwit 0 Dol phin e Sopwith Dol phin/ Sopwith Camel De Havillandj 4 S.E. 5 Sopwith Dol phin Sopwith Dol phin Sopwith Hippo B. A. T. Sopwith z| 200 b.h.p, Siddeley 200 b.b.p. Siddeley 200 b.h.p. Siddeley 200 b-h.p. Siddeley Viper Hispano 200 His- pano S. Twin Falcon Mk. 2 225 Clerget s\ 260 Fiat 240^1400 240® 1400 240^1400 240® 1400 202@l800 2io@;ooo 2x253® 2000 260^1400 Snipe De Havilland 9 Sopwith Rhine Sopwith Rhino Sopwith Rhino De Havilland 0 De Havilland 9 Sopwith Dol phin h Sopwith Dol phin * Sopwjth Dol phin j Sopwith Snipe Sopwith Snipe Bristol Fighter De Havilland 9 i| 200 His pano S. 200 His pano S. 1 jo Mono r.nnmf . *J Roils Eagle 8 Viper Hispano 200 His pano S. 200 His-1 pano S. 2] 220 Clexget 100 Mono] Gnome 438 258 258 •»» 438 249 258 2IO@2000| 258 2IO(gj2000 210@ 2000 I54@I225 360® 1800 202® l800 2IO@2000 438 438 438 438 249 405 868 98 m-5 1505 107 1475 105 1095 86 1885/1895 115 1345 127-5 1970 121-5 1915 102 101 975 II7-5 97-5 93 W9 119 114 9-7| 200 B.R. 2 260 Fiat 200 b.h.p. Siddeley 200 b.h.p. Siddeley 200 b.h.p. Siddeley 200 b.h.p. Siddeley 200 b.h.p. Siddeley 200 His pano S. ij 200 Hi-,- | pano S. 200 His pano S. 200 B.R. 2 200 B.R. 2 200 b.h.p. Siddeley 200 b.h.p. Siddeley io5@ 1250 228@I30O 260® 1400 240® 1400 240® 1400 240^1400 240® 1400 240® 1400 210'q. 2000 2I0@200O 2I0@2000 228@I3O0 228^1300 24&@ I 400; 240® 14001 300 230 274 438 (6I2)|. (612) (612) 438 438 258 258 238 274 274 405 43« 130 1840 128 1945 1135 1345 200 1205 117-5 1625 103 1490 103 1435 "4 1570 108-5 1420 "9-5 2040 1990 '"•3 »990 i*4 120 H9-5 116-5, 107 107-51 I "•7 6-7 8-7 18-2 7-41! 9-8 61 7-1 5'6 65 6-3 64 6-2 7-4 9-1 4-9 9-0 12-5 I3-5| 55o 520 460 430 810 620 250 655 900 775 960 840 870 855 885 655 17-1 17-9 20-3 21-7 n-6 I5-I 38-2 13-4 550fl6-6 103 I2-I 9-6] 405 1350 380 1330 315 i35o 290 1330 610 1720 475 1810 "5 1805 47o 123° 405 1420 703 1725 590 1725 755 "75 n-3| 660 10-8 II'O 10-6 13-4 104 1505 no 1525 no "4 99 101 10-o 95 XI-O 55 6-5 6-5 49 4-4 7-7 10-4 1040 580 380 35o 500 540 465 910: 800 800 1040J 1225 710 JOO 1575 663 1780 675 1690 683 1823 470 34-2 36-4 46-7 22-6 28-8 28-6 V7 195 23-0 179 20-9 i»o 330 270 195 240] 4=5 335 470 400 1230 S5o)i6-8| 360 8-8 16-0 248 26-8 18-6 173 20-2 103 n-7 n-7 8-8 7-4 I3'5 18-7 1075 760 1190 430 »445 210 1375 »85 1375 325 1380 385 1395 303 1360 685 1840 600 1825 600 1825 760 1190 1000 1193 550 1360 360 136S 20-2 199 28-6 2IOOO] 20000 74 7-6 22000 62 IIOOO 7-t 7-6j g-1 a-1 17500 17000 15000 14500 19000 8-o 19000 6 • 5 10500 9-2 17000 loooo|8-2 140 139 M-9 149 98 12-5 15-8 20-8(370 42U 405 195 43-oj 85 17-6 32-3! 400 2'5 36-7 49*5 19500] 21000 8-o 7-8 77 7-2 I45O0J3-3 19000 7-1 105-4 98-6|355 93-41292 12000I 85 176 13-3 25-2 38-8 400 710 320 160 17500 8-2 12000 5-9 5-9 I45°O|5*0 16300 14500 19000 18 joo 18500 19300 3'9 91 9-3| 94 99 98 9-6 95 I2'0 8-6 13-9 IJ-O 13-Oj 12-8 97-8 t&6 290 M-dhjol 7-6| 94 7-8 7-» 7-2 16500] 6-9 7-6] 9-6 97 8-6 335i 3342 3564 3564 1980 2630 8017 2590 3600 1911 1959] •441 2234J 2225 2235 2225 1733 5284 930| 3576J2509] 1988 2OO3 1990 259° 572 572 572 572 345 1730 230 322 185 »8j 407 407 360, god 360 360 ISO 192J360 46J 363 183 IOI I rj« 101 183] 42 6 42 6 42 6 42 6, 28 o 1481 laooj 866| 1950 3600 2460J 3590 3590] 3061 n-7 13-8 87-9 2183 2183 2183 180 1970 2008 .. 2018 1964)^212 386 164 393 507J 507, 465i 540 36c. 360 ISO ISO 180 3*0 180 ISO 1S0 363 SO 321 185 53» 30 6 30 6 30 6 30 6 " 4 39 3|a4 9 74 10I 42 6 32 6 32 6 28 2 42 6 28 o 32 6 32 6 36o|38 xol 360 360 42 6| 30 «! 22 6 22 6 18 6 29 8 21 4 22 6 22 6 24 6 9 i 9 6 16 0 42 6| i 28IO 3316 191b 251 538J36oj 31 185 185 101 »39i 10 0 B c 8 o 8 6 11 I 9 5 a 0 8 0 8 0 180J24 8|2Q 8| 7 5 180] .. 3° 6j 41 0(30 3] <>0 360 360)42 0I30 6j 42 6 180(32 6J22 tl 3*6 180J32 6 22 6 I49JI8O|3» 6J22 6| 347 57o "l 183 185 1 bo 180 30. 360] 30 o 30 o 39 6 42 6 18 7 18 7 26 0 10 0 8 0 B 0 9 ° 9 » 9 5 30 *|l« ° NOTE.—Loading, lbs. per h.p.—Gross weight -s-actual h.p. developed at normal revs. (A suttsi R shows that rated h.p. has been used in absence of actual h.p.) Lilting surface—Surface of wings and flaps only Military load—Weight of guns, bombs, ammunition and reconnaissance load. ' Air endurance—At 10,000' altitude at full throttle including climb. Service ceiling—Height at which rate of climb is 100 ft./min. Weight empty—Includes cooling water for water-cooled engines. « With reconnaissance load and gap covered with triplex. b With reconnaissance load, but with gap open. c With 14-20-lb. bombs and gap covered with fabric. 206 d With 14-20-lb. bombs, but with gap open. r. Without cabane and Lewis gun. / Wiib cabane and Lewis gun. e Two super-imposed two-bladed D.G.li- »6io. h With 2 Vickers guns only. 1 With 2 Vickers guns and Lewis gun on top plan' j With 2 Vickers guns and Lewi* gun on cabani . Comparative performance reduced to correspond with loadings of 14 lbs. per h.p. and 7 lbs. per sq. ft
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