Main Specifications |
||
Max level speed |
≥270m/s |
|
Max working altitude |
≥12000m(altitude) |
|
Take-off altitude |
≮4500m(altitude) |
|
Ultra low altitude flight capability |
Phase height 20m, terrain following (Gobi desert terrain) |
|
Body length |
3660mm |
|
wingspan |
1732mm |
|
Body height |
576mm |
|
Max take-off weight |
≥150kg |
|
Maximum oil load |
≮40kg |
|
Max maneuvering overload |
Basic type:≥4g |
|
Large maneuver type: ≥7g (sea height: 5000m), |
||
Endurance |
≥60min |
|
Remote sensing radius |
Controlled aircraft position and the origin of distance ≮ 100 km |
|
control mode |
Program control + remote control |
|
Takeoff mode |
rocket assist |
|
recovery mode |
Parachute recovery + air bag shock absorption |
|
RCS |
≯0.01 ㎡ (head on ±30°, C, X, Ku, Ka band) |
|
Cooperative formation capability |
Fleet number |
≥6 |
Formation retention accuracy |
Level: better than 30m |
|
Mission payload |
weight |
≥20kg |
Payload type |
One or more of the following load combinations |