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Otto A.G.O. 50 hp, longitudinal section Otto A.G.O. 50 hp, cross section. The Otto A.G.O. (Aeromotor Gustav Otto) 50 hp engine was designed by Hans Geisenhof in 1911 at the Gustav Otto Flugmaschinenwerke. It had a bore and stroke of 110 mm × 150 mm (4.33 in × 5.91 in) and produced about 50 hp (37 kW) at 1,200 rpm. [2] [3]
The Continental O-170 engine is the collective military designation for a family of small aircraft engines, known under the company designation of A50, A65, A75 and A80. The line was designed and built by Continental Motors commencing in the 1940s. It was employed as the powerplant for civil and military light aircraft. [1]
The Argus 50 hp aircraft engine was developed by Argus Motoren around 1909 based upon their earlier balloon- and boat-engines. [1] [2]It had a bore of 124 mm (4.88 in) and a stroke of 130 mm (5.12 in) and produced about 45–55 hp (34–41 kW) at 1200–1300 rpm [3] [4] and was produced in two variants, with the valves and camshaft on the right [3] or on the left side [5] respectively.
Argus As 12: 16H 550 hp [4] Argus As 16: 4-cylinder inverted inline 40 hp [4] Argus As 17: 6-cylinder inverted inline 225 hp / 285 hp [4] Argus As 401: development and renumbering of the As 10 Argus As 402: [4] Argus As 403: radial engine project, not built. Argus As 410: 12-cylinder inverted V [4] Argus As 411: 12-cylinder inverted V [4]
Argus As 12 16H 550 hp [37] Argus As 16 4-cylinder horizontally-opposed 35 hp [39] Argus As 17; Argus As 014 (aka "Argus 109-014") – pulse jet engine for V-1 flying bomb and Tornado boat; Argus As 044 [37] Argus As 16 4-cylinder inverted inline 40 hp [37] Argus As 17 6-cylinder inverted inline 225 hp / 285 hp [37]
The Otto A.G.O. (Aeromotor Gustav Otto) 80/100 hp engine was designed by Hans Geisenhof in 1911 at the Gustav Otto Flugmaschinenwerke.It had a bore and stroke of 140 mm × 150 mm (5.51 in × 5.91 in) and was rated at 80 / 100 hp (60 / 75 kW) with a normal speed of 1,200 rpm.
The L550E is an air-cooled horizontally-opposed 550cc four-cylinder two-stroke petrol engine developing 37 kW (50 hp) at 7500 rpm which can drive a propeller either directly or geared. It employs a single magneto ignition, four carburettors , and is lubricated by oil mixture lubrication with a fuel to oil ratio of 25:1 for mineral oil or 50:1 ...
Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio
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