|
|
Please note!
These figures have been calculated on computer and
are definately not accurate.
The computer, ie, does not know what type of engine
you are using.
A 50hp Rotax will outclimb a 50 Hp VW, but the VW
can outcruise the Rotax etc.....
Final performance figures will only be available
after proper flight testing.!!
Please keep this in mind when reading these predictions.
|
Dims and stats (estimated) |
metric |
imperial |
|
Length |
4.5 m |
14.75' |
|
Wing Span |
10.5 m |
34.4' |
|
Wing Area |
12.81 m2 |
137.6 sqft |
|
Aspect Ratio |
8.6 |
8.6 |
|
All-up weight |
450Kg |
990 lbs |
|
Powerplant: |
~37Kw |
~50 Hp |
|
Aircraft Cdo |
0.031 |
0.031 |
|
Performance Estimates (Calculated) |
metric |
imperial |
|
Max level speed: S/ L |
168km/h |
105mph |
|
Cruise speed, S/L 65% power |
146km/h |
91 mph |
|
Max level speed , 5000' ASL |
167km/h |
104 mph |
|
Cruise speed, 5000' ASL, 65% power |
144 km/h |
90mph |
|
Stall speed S/L |
60 km/h |
38mph |
|
Stall speed ,5000' ASL |
59 km/h |
37 mph |
|
Rate of Climb,S/L |
309 m/min |
1016fpm |
|
Rate of Climb,5000' ASL |
260m/min |
852 fpm |
|
Climb speed S/L |
80 km/h |
50 mph |
|
Climbspeed ,5000' ASL |
86 km/h |
53 mph |
|
Take-off S/L |
metric |
imperial |
|
Ground run concrete |
129 m |
423' |
|
T-O to 15.3m (50') |
330 m |
1081' |
|
Ground run grass |
155m |
508' |
|
T-O to 15.3m (50') |
356 m |
1167' |
|
Take-Off: 5000' ASL: |
metric |
imperial |
|
Ground run concrete: |
182 m |
596' |
|
T-O to 15.3m (50'): |
465 m |
1526' |
|
Ground run grass: |
230 m |
754' |
|
T-O to 15.3 m (50') |
512 m |
1678' |
|
Landing S/L: |
metric |
imperial |
|
Landing distance from 15.3m (50') |
259 m |
849' |
|
Ground run |
80 m |
262' |
|
Landing, 5000' ASL: |
metric |
imperial |
|
Landing distance from 50' |
277 m |
908' |
|
Ground run: |
93m |
305' |