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Vega ST 87
The
Vega ST 87 is a side by side two seat, low wing aircraft designed by
René Stern. Construction materials are wood & fabric. The landing
gear may be built as a fixed trigear or fixed tailwheel.
specifications
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
108 to 125 HP
x
23 ft.
9 ft.
25 ft.
108 sq. ft.
x
1035 lbs.
x
1600 lbs.
30 gal.
750 m.
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performance
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
1400 ft.
To 50 ft.
788 ft./min.
150 mph.
x
1500 ft.
Over 50 ft.
13,000 ft.
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limiting and recommended speeds
design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
x
168 mph.
62 mph.
75 mph.
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All specifications are based on manufacturer's
calculations
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