Long-endurance operations
A project-context category for requirements discussion.
UAV SOLUTIONS
Organise aircraft and operating requirements before comparing published data and opening an engineering discussion.
01 / MISSION CONTEXT
A project-context category for requirements discussion.
A project-context category for requirements discussion.
A project-context category for requirements discussion.
A project-context category for requirements discussion.
A project-context category for requirements discussion.
02 / SELECTION INPUTS
A single power, displacement or thrust value is insufficient to confirm compatibility.
03 / FROM REQUIREMENT TO REVIEW
04 / PUBLISHED DATA
| Field | ZT-T170 | ZT-T222 | DLE170 | DLE222 |
|---|---|---|---|---|
| Configuration | Twin-cylinder, air-cooled, two-stroke gasoline engine | Four-cylinder, air-cooled, two-stroke gasoline engine | Twin-cylinder two-stroke gasoline engine | Four-cylinder two-stroke gasoline engine |
| Displacement | 170 cc | 222 cc | 170 cm³ | 222.5 cm³ |
| Rated power | 18.1 hp / 13.3 kW | 20.9 hp / 15.3 kW | 10.77 kW @ 7,500 rpm | 11.76 kW @ 7,523 rpm |
| Engine weight | 3.93 kg | 4.86 kg | 3,620 g | 4,860 g |
| Propeller data | 30 × 12 / 32 × 10 | 32 × 10 / 32 × 12 / 34 × 10 | 30 × 12 / 32 × 10 | 32 × 10 / 32 × 12 / 34 × 10 |
ENGINEERING SUPPORT