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111.85 kW (150 hp) 300 built in France, 300 built in Russia. Powered the Voisin type LA 5 and Farman HF.27: Salmson R9 9-cyl radial 1915 125 mm (4.921 in) 140 mm (5.512 in) 15.46 L (943.43 cu in) 111.85 kW (150 hp) – 119.3 kW (160 hp) at 1300rpm 50 built in France, 300 built in Russia.
150 kW (200 hp) 9P 70 kW (94 hp) 9Y 11B 12C 190 kW (250 hp) W-12 engine 18Z 450 kW (600 hp) Salmson-Szydlowski SH18 18 cylinder air-cooled 2-stroke radial.
SM UB-88 in Miami, Florida (c. 1919) SM UB-88 in the U.S. c. 1920. UB-88 was surrendered to the United States on 26 November 1918 in accordance with the requirements of the Armistice with Germany.
Most French-built Type H aircraft had water-cooled V-8 Hispano-Suiza 8A variants with powers of 150 or 170 hp (110 or 130 kW), though a minority had 160 hp (120 kW) Lorraine 8Ns. [1] Some Italian built Type Hs also used the higher-power Hispano motor but more had 180 hp (130 kW) Isotta Fraschini V.4 B or 150 hp (110 kW) engines of the same make ...
The more powerful version will produce a 150-kW beam capable of knocking down missiles with the weight and size requirements for fitting onto fighter aircraft or a Humvee. In mid 2008, Jane's International Defence Review quoted the US military that the program is on schedule to meet this ground test. Phase 4 of the program, involving outdoor ...
The first three batches were equipped with the 150 hp (110 kW) Benz Bz.III engine. The last two batches, 35 aircraft in total, were equipped with the 160 hp (120 kW) Maybach Mb.III engine. [ 7 ] The first four batches were armed with one fixed Spandau machine gun, mounted on the starboard side of the nose.
Originally rated for 150 hp (112 kW) at 1,600 rpm with a displacement of 14.6 L (891 cu in) and a weight of 240 kg (529 lb). [3] Maximum power 201 hp (150 kW). [5] SPA 6A Semi-Super-Compressed Identical to the normal 6A, but with the cylinder bore increased to 137 mm (5.39 in), and with a capacity of 15.03 L (917 cu in).
On 27 October 1977, the first prototype (registration D-EATJ), powered by a pair of EA871 110 kW (150 hp) NSU Wankel engines, made its maiden flight. [3] The EA871 engine installation proved to be troublesome, thus the second prototype ( D-EATI ) was furnished with a single 310 kW (420 shp) Allison 250-C20B turboshaft engine, making its first ...