StarLite Warp
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The Star-Lite Warp 1-A is an American homebuilt aircraft that was designed and produced by Star-Lite Engineering of
Englewood, Ohio Englewood is a city in Montgomery County, Ohio, and a northern suburb of Dayton. The population was 13,465 at the time of the 2010 census. It is part of the Dayton metropolitan area. History Although Englewood was not actually founded until 1841 ...
, introduced in 1996. When it was available the aircraft was supplied as a kit for amateur construction.Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition'', page 257. BAI Communications, 15 July 1998.


Design and development

The aircraft was designed to comply with the US
FAR 103 Ultralight Vehicles Ultralight aircraft in the United States are much smaller and lighter than ultralight aircraft as defined by all other countries. In the United States, ultralights are described as "ultralight vehicles" and not as aircraft. They are not requ ...
rules, including the category's maximum empty weight of . The aircraft has a standard empty weight of . The Warp 1-A features a cantilever mid-wing, a single-seat enclosed cockpit under a bubble canopy, fixed tricycle landing gear with wheel pants, a boom-mounted T-tail and a single pod-mounted engine in
pusher configuration In an aircraft with a pusher configuration (as opposed to a tractor configuration), the propeller(s) are mounted behind their respective engine(s). Since a pusher propeller is mounted behind the engine, the drive shaft is in compression in nor ...
. The aircraft is made from composites. Its span wing is made with an aluminum spar and
S-glass Fiberglass (American English) or fibreglass (Commonwealth English) is a common type of fiber-reinforced plastic using glass fiber. The fibers may be randomly arranged, flattened into a sheet called a chopped strand mat, or woven into glass cloth ...
vinyl-ester resin, is detachable for ground transport or storage and has a wing area of . The standard engine used is the Rotax 503 two-stroke powerplant. The Warp 1-A has a typical empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload for the pilot and baggage is . The standard day, sea level, no wind, take off and landing roll with a engine is . The manufacturer estimates the construction time from the supplied kit as 100 hours.


Operational history

In March 2014 one example, the prototype, was
registered Registered may refer to: * Registered mail, letters, packets or other postal documents considered valuable and in need of a chain of custody * Registered trademark symbol, symbol ® that provides notice that the preceding is a trademark or service ...
in the United States with the Federal Aviation Administration as an Experimental - Amateur-built, although its registration expired in June 2013.


Specifications (Warp 1-A)


References

{{reflist


External links


Official website archives
on Archive.org
Photo of the prototype Warp 1-A
Warp 1-A 1990s United States sport aircraft 1990s United States ultralight aircraft Single-engined pusher aircraft Mid-wing aircraft Homebuilt aircraft