H3 Pegasus
experimental aircraft pictures, H3 Pegasus amateur built aircraft
specifications, H3 Pegasus homebuilt aircraft specifications and photographs,
Ultralight News newsmagazine.
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Single place Part 103 ultralights in the United States are defined as single
place ultralight aircraft that weigh 254 lbs or less, have a stall speed
not more than 24 knots, a top
speed of 55 knots, and carry no more than 5 gallons of fuel. To fly a
legal Part 103
ultralight aircraft in the United States the pilot does not require a
pilot license.
Single place aircraft weighing more than 254 lbs. in the U.S. require a
pilots license and must be built as experimental, amateur built,
homebuilt aircraft. These include weight shift aircraft, more commonly
known as trikes, powered parachutes, and powered para-gliders.
Single place ultralights in Canada can weigh up to 1200 lbs. and an
ultralight pilots license is required to fly them.
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H3 Pegasus pictures and
specifications, images of the
H3 Pegasus amateur built experimental homebuilt aircraft
specifications and data.
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H3 Pegasus pictures, images
and specifications for the
H3 Pegasus
amateur built experimental homebuilt aircraft.
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H-3
Pegasus Experimental Amateur Built Aircraft Specifications |
Airframe
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Wing Span |
25 Feet |
Fuselage Length |
15 Feet |
Empty Weight |
305 to 345 lbs |
Wing Area |
110 Sq Ft |
Power |
Engine |
28 to 55 HP |
H-3
Pegasus Experimental Amateur Built Aircraft Performance Specifications |
Stall Speed
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30-41 mph |
Cruise Speed |
65-80 mph |
Top Speed |
80-95 mph |
Gross Weight |
555-595 lbs |
Design Load @500
lbs gross wt |
+5, -3.5 |
Climb Rate |
500 to 700 fpm |
Fuel Capacity |
5 to 7.5 gallons |
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H3 Pegasus
Experimental Aircraft |
H3 Pegasus
Experimental Homebuilt Aircraft |
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To view the
pictures, images of the H3 Pegasus click on the smaller
images and they will enlarge. To return to the index page for the H3 Pegasus click on H3 Pegasus Index link, to view
video of the H3 Pegasus click on the Video link, to
return to the Main Index click on the UltralightNews link. |
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