Pegasus PAL 95
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The Pegasus PAL 95 is a twin cylinder,
horizontally opposed A flat engine is a piston engine where the cylinders are located on either side of a central crankshaft. Flat engines are also known as horizontally opposed engines, however this is distinct from the less common opposed-piston engine design, wh ...
aircraft engine that was developed by Pegasus Aviation (NZ) Ltd of
New Zealand New Zealand ( mi, Aotearoa ) is an island country in the southwestern Pacific Ocean. It consists of two main landmasses—the North Island () and the South Island ()—and over 700 smaller islands. It is the sixth-largest island count ...
for use in
ultralight aircraft Ultralight aviation (called microlight aviation in some countries) is the flying of lightweight, 1- or 2-seat fixed-wing aircraft. Some countries differentiate between weight-shift control and conventional three-axis control aircraft with ailer ...
. The engine is no longer available.Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page G-9 Cybair Limited Publishing, 2001.


Development

Designed to fill a similar market segment as the similar configuration and output
HKS 700E The HKS 700E is a twin-cylinder, horizontally opposed, four stroke, carburetted aircraft engine, designed for use on ultralight aircraft, powered parachutes and ultralight trikes. The engine is manufactured by HKS, a Japanese company noted for ...
, the PAL 95 produces at 5200 rpm. The PAL 95 has a computer-controlled engine management system that controls both the
fuel injection Fuel injection is the introduction of fuel in an internal combustion engine, most commonly automotive engines, by the means of an injector. This article focuses on fuel injection in reciprocating piston and Wankel rotary engines. All comp ...
system and the ignition timing, giving automatic altitude-compensated mixture control. The pistons are forged and ceramic coated. The intake valves are made from nickel-steel and the exhaust valves from
stainless steel Stainless steel is an alloy of iron that is resistant to rusting and corrosion. It contains at least 11% chromium and may contain elements such as carbon, other nonmetals and metals to obtain other desired properties. Stainless steel's corros ...
. The engine was supplied with an electric starter and an exhaust system by the factory as standard equipment. Speed reduction is via a standard twin cog-belt system, with harmonic dampening on the crankshaft pulley. The initial TBO was estimated by the manufacturer as 1500 hours.


Specifications (PAL 95)


See also


References

{{Reflist 1990s aircraft piston engines