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Glasair
1
The Glasair was the first kit aircraft that used
moulded surfaces rather than the Rutan method of construction. The
original Glasair 1 required a very long time to construct. The original company, Stoddard
Hamilton, (named after the late designer) went into liquidation due
to reasons outside the Glasair range. Fortunately the company was
purchased by aircraft enthusiast
Thomas W. Wathen and is now going from
strength to strength. The Glasair range included a taildragger
version (TD), fixed trike (FT) and a retract (RG). Wing extensions
were available which improved performance at higher altitude but
reduced g loadings.
The Glasair is the ideal long distance fast personal
aircraft.
These aircraft are not only extremely strong, but fly
better than almost any experimental. They are renowned for their
handling characteristics. In addition, the resins used very rarely
cause allergy problems for builders.
Performance is varied according to choice of engine, which can range
from 160 hp to 200 hp.
specifications and performance figures for 200 hp variant with
extended fuel tanks and no wing extensions
specifications (RG)
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
Lyc IO 360 A1B 200 hp
3 blade Hoffmann VP wood blades
19ft 6ins
6ft 2 ins
24ft 4ins
81.3 sq ft
2
1368lbs
632lbs
2000lbs
(In USA
2200lbs allowable)
61.4 Imp gal.
1177
Miles |
performance
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
400m
1500 ft/min
260
mph
175 kts
IAS
500m
19,000ft |
limiting and recommended speeds
design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
145 mph
260 mph
65 mph
90 mph |
All specifications are based on manufacturer's
calculations
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