|
Jodel D150 Mascaret Series
performance
and specifications
Specifications with 100hp O-200 engine
Overall dimensions: |
|
|
Length |
20.6 ft |
6.3 m |
Wing span |
26.7 ft |
8.15 m |
Weights and loadings: |
|
|
Empty weight (with oil) |
900 lbs |
410 kg |
Max Take off weight |
1585 lbs |
720 kg |
Usefull load |
685 lbs |
310 kg |
Bagage shelve |
130 lbs |
60 kg |
Power loading |
15.9 lbs/hp |
7.2 kg/hp |
Fuel capacity (wings) |
2 x 9 imperial gal |
2 x 40 l |
Fuel capacity (rear) |
24 imperial gal |
110 l |
Other specs: |
|
|
Gear |
Tailwheel |
|
Seats |
2 |
|
Controls |
Stick and rudder |
|
Material |
Wood and fabric |
|
Engine: |
|
|
(D150) |
100 hp |
Continental O-200 |
(D150 A) |
105 hp |
Potez 4E20 |
(factory experiment) |
135 hp |
Continental O-200 |
(homebuilt) |
150 hp |
Lycoming O-320 |
Fuel Continental |
80/87 octane |
Mogas permitted |
Fuel Potez, Franklin, Lycoming |
100/130 octane |
Mogas not permitted |
Fuel burn (O-200), 75% pwr |
5.5 gph |
21 litre/hour |
Fuel burn (O-200), 55% pwr |
4 gph |
15 litre/hour |
Performance: |
|
|
Max speed, sea level |
165 mph |
265 km/h |
Cruise speed |
130 mph |
210 km/h |
Stall speed (with flaps) |
38 mph |
60 km/h |
Climb rate |
630 fpm |
3.2 m/s |
Service ceiling |
15000 ft |
4500 m |
Endurance |
|
10 hours |
|
|