DLG-mini X Tail

The DLG-mini is defined as an entry-level hand-launch glider. Designed in accordance with mainstream DLG principles to suit a variety of flying environments, it is a high-performance model manufactured using modern metal molds and a high-temperature molding process.

SPECIFICATIONS:

Preferences                    Motorless

Wing span                     950mm

Length                           640mm

Wing area                     12.6dm2

Wing chord                   150mm

Empty weight               110g

Flying weight                160g

Wing airfoil                   SY II series

CG                                 45mm from leading edge

Tow hook setting            NO

Ailerons                          YES

Elevator                         YES

Rudder                          YES

Flaps                             NO

Required Radio             4 channels

Recommend equipment configuration for a motorless version basic configuration

Servos                           EMAX ES9052 *4

Settings:

Ailerons: Up 12mm, Down 8mm

Elevator: +10mm / -10mm

Rudder: +15mm / -15mm

Butterfly (Crow): Ailerons down 45°, Elevator -4mm

SPEED: Ailerons up 2mm; adjust elevator based on actual flight attitude

SPEED: Ailerons up 2mm; adjust elevator based on actual flight attitude

CRUISE: Ailerons 0, Elevator 0

THERMAL: Ailerons down 3–6mm; adjust elevator based on actual flight attitude

ZOOM: Ailerons up 1.5mm; adjust elevator based on actual flight attitude

PRESET: Ailerons down 1–2mm

Another important thing about the surface of the glider: this RCRCM glider is fully moulded. Mould precision ensures that each glider has a complete aerodynamic layout but in the process of composite production, there is a slight chance of very tiny air bubbles or slight cloth grain. In the unlikely event that these small imperfections exist, they do not affect the structural strength or flight performance.

Glider long term storage: Hang glider vertically to reduce the stress on the glider surfaces to avoid deformation that could adversely affect flight performance and trim.