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Crossfire von Peter Germann
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Airplane

Crossfire            

T/O weight

63.8 oz or 1’810 Grams

Area (Wing & flaps)

694 sq.in or 44.7 dm

Span

1’540 mm (60.6 in)

Wing airfoil

NACA 0018 max 2.32 in or 59 mm. &  flatplate flaps  8 mm or 0.3 in

Flaps hingeline sweep

none

Hingeline-hingeline

485 mm or 19.1 in

Empennage airfoil

NACA 0012  max, 0.75 in or 19 mm. Elevators integrated

Stabilizer A.o.A.

+/- 0°

Motor thrust angle

+/- 0°

Nose length

275 mm or 10.8 in  Backplate – leading edge (centre)

Motor axis above wing c.l.

0.8 in or 20 mm

Stabilizer c.l. above wing c.l.

1.8 in. or  45 mm

Rudder

Neutral, not adjuststable

Graphics design

Claus Maikis

 

 

Power Train

 

Motor

AXI 2826/12  760 Kv & cooling fan COOL1

ESC

Castle Creations Phoenix Edge lite 75 A  Firmware V 4.20 (Beta)

Mode

Control Line / brake on, high governing mode, auto-lipo off. Cutoff set to 15.0V

Timer

Hubin FM-9

Battery LiPo

Thunder Power G8 Pro Force G8 2’700 mAh 5S 70C

Spark protection

Jeti 4 mm female on + of batteries.

Propeller

APC 13 x 5.5 EP (Pusher)

 

 

Bench Trim

December 18 2014

C.G.

7.8 in or 198 mm from hingeline fwd

Leadout Center

1 in or 26 mm. rear of C.G.  6.77 in or 172 mm from hingeline fwd.

Tip weight

Outer tip 1 oz or 28 Grams heavier

Elevators / Flaps throw

45° / 30°

Hinge seal

none

Nose trim weight

0

Tail trim weight

0

Battery trim position

Middle  of +/- 20 mm (0.8“) adj. range

Lines

0.015” x 64 ft or 19.5 m (eye-eye)

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