Search results
Results from the WOW.Com Content Network
The prototype of the Robin HR100 was the prototype DR253 Regent which was rebuilt with metal wings and powered by a 180 hp (134 kW) Lycoming O-360 engine. It first flew on 3 April 1969 as the Robin HR100/180. The HR100 is a low-wing cantilever monoplane with a conventional cantilever tail unit and a fixed tricycle landing gear.
Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [e] Oxidiser: fuel ratio Aeon 1 USA: Relativity Space: Terran 1: Retired 1st CH 4 / LOX: Gas generator: 310: 86,740 (SL) [64] Aeon 1 Vacuum USA: Relativity Space: Terran 1: Retired 2nd CH ...
In 1983, a marketing agreement was reached between Avions Robin and SOCATA, the light aircraft subsidiary of Aérospatiale to market the R 3000 series. This led to the planned higher power versions being abandoned, with engines limited to 119 kW (160 hp) or less to avoid competition with Socata's own TB series.
For example: the -18W was a "C" series engine, built from 1945, whereas the -21 was a "B" series engine, built from 1943. Until 1940 the armed forces adhered strictly to the convention that engines built for the Army Air Forces used engine model numbers with odd numeric suffixes (e.g.: -5), while those built for the US Navy used even (e.g.: -8).
3 Specifications (R.1180) 4 ... The Robin R.1180 Aiglon is a French four-seat touring and training monoplane ... Lycoming O-360-A3AD or a Lycoming O-360-A3A engine.
(These specifications are for the original R22, which is no longer in production. Later variants have different specifications.) Data from Robinson R22 Pilot's Operating Handbook., [13] R22 Introduction and Specifications [33] General characteristics. Crew: 1/2; Capacity: 1/0; Length: 28 ft 8 in (8.74 m) Height: 8 ft 11 in (2.72 m)
It was a modification of the Pratt & Whitney J52 turbojet engine which powered the US Navy A-6 Intruder and A-4 Skyhawk attack aircraft. Eight models comprise the JT8D standard engine family, covering the thrust range from 12,250 to 17,400 pounds-force (54 to 77 kN), and power the 727, 737-100/200, and DC-9.
The Lycoming R-680 is a nine-cylinder air-cooled radial engine, the first aero engine produced by Lycoming. The engine was produced in two types, the E and B series; both are essentially the same. The B4E was available in a trainer version with a front exhaust collector "ring" for use without cylinder air baffles.