Powered by a license-built Cirrus engine, and at least six of these aircraft were supplied to the RCAF
Piston
Curtiss V-8
The 1912 Curtiss V-8 aero engine was a water-cooled eight-cylinder Vee producing 75-80hp. It was basically the same as the O/OX series.
Curtiss V-4
The circa 1911 Curtiss V-4 aero engine was a water-cooled four-cylinder Vee producing 40-60hp from 1649.34ci with a dry weight of 1,086 lb.
Curtiss R-1454
The Army issued a specification for a new engine, known as the R-1454, on 15 Aug 1923. Development of the engine itself had been carried out by the Army through Wright, Lawrance, and an independent engineer, S D Heron, and had been through many changes, to the cylinders in particular. The fixed-price contract was won by Curtiss, following its bid on 13 Nov 1923, and was for the construction of three engines with an option for three more. The first engine was delivered in Sept 1924 and it gave up to 405hp @ 1650rpm. A modified cylinder developed by Heron (Type M) was fitted to the engine, and the Army instructed Curtiss to proceed with the other engines called for under the contract in Feb 1926.
Output: 400hp
Capacity: 1454ci.
Curtiss VX
The 1916 Curtiss VX was as the Model V with some minor changes. They produced 180hp@1400rpm.
Curtiss V-1550
The 1926 Curtiss V-1550 12-cylinder Vee was an enlarged D-12. They produced 575-600hp and received ATC 6.
Curtiss OXX-2 / OXX-3
The 1916 Curtiss OX-2 aero engine was a water-cooled eight-cylinder V which produced 100hp from 567.44ci and a dry weight of 401 lb.
Except for a bigger bore, it was almost identical to the OX.
Curtiss OX-2
The 1913 Curtiss OX-2 aero engine was a water-cooled eight-cylinder V which produced 85-90hp@1200rpm from 502.64ci. The dry weight was 390 lb and it featured a Bosch magneto, Schebler carburetor.
Curtiss O
The 1912 O model aero engine was a water-cooled eight-cylinder V which produced 75hp@1100rpm.
It was an improved Model L, refined again as the OX line.
Curtiss E-8
The 1909 Curtiss E-8 was a 785.4ci 4-cylinder water cooled aero engine. A double-row version of the E-4. It produced 100hp@1500rpm with a dry weight of 350lb.
Awarded top prize at 1909 Rheims air meet.