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Aviation History
1920
1920 - 0441.PDF
MULTI-SEATED MACHINES. Type. Engine. ft 8-6 '8 Speed in m.p.h. and r.p.m. at 10,000 ft. -H> < 0 S iO Time in mins., rate of climb in ft. per min., and r.p.m. at 10,000 ft. 6,500 ft. 10,000 ft.' H 15,000 ft s o 1-1 Onft 60 a .s-e Weight. s ftS W S fa riO o •a •fi l 14 H M-lO > 2 1 F.E. 4 (P. 3) .. Avro-twin (T. 3) Avro-Twin (T. 3) De H. 10 (T. 3) De H. 10 (T. 3) De H. 10 (T. 3) De H. IOA (T. 3) Handley Page (T. 4) 0.400 BristolBraemar (T.&P. 4) Handley Page (T. & P. 6) V. 1500 2 R.A.F. 5 . 2 190 Rolls R. 2 200 b.h.p. . 2 400 Libertys 2 400 Libertys 2 400 Libertys 2 400 Libertys 2 275 Rolls II 4 Sid. Pumas 4 Rolls, Eagle 8 84-3 94 106 "3-5 120 - 120 130 91 -5 107 97 at G.L. 8,000 10,000 10,000 3,000 3,000 5,000 5,000 5,000 119 128 101 89 106 "5 116-5 124 80 95 93 i°5 no 117 220 735 920 863 965 1,020 1,170 495 760 47n-4 9-1 9-3 8-2 7-7 6-4 16-0 18-5 55 430 555 56a 650 695863 215 295 220 21-7 iG-5 16-6 14-6 13-4 n -o42:6 31-7 260 400 403 473 525 675 Ir3 160 34- 35- 29- 26- 23 • 165 2 75380 7 l6,O00 20,030 l8/>33 19,53° 2O,5O3 19,003 14,000 11,50 12,800 it. 6,600 14,000 17,000 16,100 17,400 17,500 10,003 13,820 8,750? Weight empty includes cooling water for water-cooled engines. SEAPLANES AND SHIP AEROPLANES 6 b 8 8 8 8 12 14 , ,3">9 ,05 > ,533 ,530 ,500 ,5" ,233 .573 ,7O3 4.376 —- 5,630 —• —- 5,75' 8,483 9,878 16,210 1 1 1 1 2 3 4 ,365 ,120 —. ,435 —• — ,756 ,833 .635 ,290 40 273 — 925 — — 454 203 345 3,120 54° 54° 54O 54° 54° 720 720 1,080 lbs. 1.945 r,933 ? 2.900 2.915 2,915 2,750 3,75o 4,700 8,490 516 6.17 it.17 7.18 8 18 8.18 9.18 9.17 10.18 9.18 U. M. M. M. M. M. M. M. M. M. Type •;•• Engine Normal b.h.p. and r.p.m. at G.L. a i 3 cn Speed M-l s- 4•< in <8in knots -P 0 ' 0 M Time in mins., and rate of climb in ft. per min. •2,003 ft. 4 ' 6,500 ft. H 1\ 10,000 ft: AirEn- durance OB a Weight. O ft W Loading. 8" Ship Aeroplanes— Parnall Panther (T 2) Sopwith Camel (T 1) Sopwith Torpedo (T 1) Float Seaplanes— Fairey Campania T Fairey 3B (T 2) .. Sunbeam Maori Fairey 3c (Normal Rolls Eagle 8 load) (T 2) Fairey 3c (Over load) (T 2) Short Improved 184 (T 2) Boat Seaplanes— F.2A (T 4) F. 3 (Normal load) (f 4) F. 3 (Over load) (T 4) F.5(Normal load)(T4) F/5 (Overload) (T 4) H. 16 (T 4) NOTE.—Loading lbs. per h.p. .. Lifting surface Military load Type : T = Tractor; 230 B.R.2 150 B.R.I Sunbeam Arab 275 Rolls, Mk.I Rolls Eagle 8 260 Sunbeam 2 Rolls Eagle 8 2 Rolls Eagle 8 2 Rolls Eagle 8 2 Rolls Eagle 8 .2 Rolls Eagle 8 2 Rolls Eagle 8 228 at 1,300 150 at 1,250 207 at 2,000 307 at 1,800 265 at 2,100 359 at 1,800 359 at 1,800 265 at 2,100 2X345 at 1 2 x 345 at 1 2 x 345 at 1 2 X 345 at 1 2 x 345 at 1 2X345 at 1 800 800 ,800 ,8oo ,800 325 229 568 654 57°476 476 680 1,133 1,43° 1,43° 1,409 1,409 1,200 108 90-5 76 79 96 87-5 73 83 79 78 89 88-5 85-5 94 105-5 89 72 75-5 93 83 72 77 74-5 75-5 86 80-5 83-5 89-5103 85 — 89 — 70 7° 78-5 80 2-3 i-8 4-0 5-6 4-3 2-3 3-7 6-3 3-8 5-4 7-8 4-0 5-3 3-7 795 1,278 466 307 410 794 500 300 470 333 230 462 352 512 9-3 6-'2 15-7 28-5 19-5 9-3 16.5 26-3 i6-7 24-0 41 -o 16-1 22 '5 14 -6 545 752 303 • 120 210 5i° 246 165 252 163 75 290 193 335 17-1 ri-4 3V° 18-0 44-0 — 395 32-5 28-0 345 541 176 332 48 86 163 4jatio,ooo' 4 at 10,000' 4* 5$- at 6,000' 5 at 6,000' 4* at 1,000 at 2,000 Gross weight -t- actual h.p. developed at normal revs. Surface of wings and flaps only. Weight of guns, bombs, ammunition and reconnaissance lftad. P = Pusher. The figure in brackets indicates number of seats. at 6,000 at 6,000 198 6 at 2,000 Air endurance .. Service ceiling .. Weight empty • 18-inch torpedo. 14,500 17,500 12,000 7,000 9,000 15,000 8,500 9,000 9,5°°8,000 6,000 11,500 9,000 12,500 2,595 i,53o 3,883 5,4°6 5,083 4,800 5,O39 5,123 10,978 12,235 13,281 12,268 13,306 10,670 1,328 1,036 2,199 3,6i3 3,423 3,392 3,549 3-479 7,549 7.958 7,958 8,023 8,023 7.363 541 223 4°5 783 610 878 883 637 2,124 2,096 3.H2 2,097 3,121 2,115 366 9i•1,099 650 690 170 247 647 585 ti,46i ti,46i ti,428 fi.442 472 360 180 180 360 360 360 360 360 720 720 720 720 720 720 8-0 67 6-8 8-3 8-9 IO-I IO-6 7'5 9-7 S-55 93 8-79-4 8-9 n-4 10-2 18:75 17-6 19-2 13-4 14 o 19-9 15-917-7 19-25 17-8 5/ 10/17 6/18 6/17 10/18 10/18 3/19 9/17 3/18 4/18 4/18 8 At 10,000 ft. alt., at full throttle, including climb. Height at which rate of climb is 100 ft. min. Includes cooling water for water-cooled engines, f With four 230-lbs. bombs.
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