Apogee - · PDF file0 10 20 in 36 12 RC HLG Mark Drela 8 . 8 . 1999 Sh = 15.2 sq in Sv = 8.0...
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0 10 20 in 36 12 RC HLG Mark Drela 8 . 8 . 1999 Sh = 15.2 sq in Sv = 8.0 sq in V = 4 - 11 m/s = 9 - 26 mph Re = 7 - 21K /in CL = 0.8 - 0.1 L/D = 16 - 7 AG-04 6.3% t 1.7% c Apogee "36" Avia "Skinny" carbon boom Span: 36 in Area : 166 sq in Mass: 3.6 oz 2 HS50 servo 11.0 g Hitec 555 RX 15.0 g 3 NiCd 50mAh 11.0 g Wiring 2.0 g Wing 46.0 g Fuse 8.0 g Boom 3.0 g Tail 4.0 g Rods 1.0 g TOTAL 101.0 g AG-09 4.8% t 2.0% c HT-05 4.8% t 0.0% c 0.012" wire pushrods polyethylyne housings +/-27 deg max throw before mixing 0.46" Spyder Foam 32 cu in vol. 1-3 layers 0.75 oz glass, +/-25 deg orientation Kevlar 120 fuselage 2,3 layers 34 sq in surf. Spyder Foam 1.6 cu in vol. 1 layer 0.75 oz glass, +/-20 deg front +/-45 deg elevator
Transcript of Apogee - · PDF file0 10 20 in 36 12 RC HLG Mark Drela 8 . 8 . 1999 Sh = 15.2 sq in Sv = 8.0...
0 10 20 in
3612
RC HLG
Mark Drela 8 . 8 . 1999
Sh = 15.2 sq in
Sv = 8.0 sq in
V = 4 − 11 m/s = 9 − 26 mphRe = 7 − 21K /in
CL = 0.8 − 0.1L/D = 16 − 7
AG−046.3% t1.7% c
Apogee "36"
Avia "Skinny"carbon boom
Span: 36 inArea : 166 sq inMass: 3.6 oz
2 HS50 servo 11.0 gHitec 555 RX 15.0 g3 NiCd 50mAh 11.0 gWiring 2.0 g
Wing 46.0 g Fuse 8.0 g Boom 3.0 g Tail 4.0 g Rods 1.0 g
TOTAL 101.0 g
AG−094.8% t2.0% c
HT−054.8% t0.0% c
0.012" wire pushrodspolyethylyne housings
+/−27 deg max throw before mixing0.46"
Spyder Foam 32 cu in vol.1−3 layers 0.75 oz glass,+/−25 deg orientation
Kevlar 120 fuselage2,3 layers34 sq in surf.
Spyder Foam 1.6 cu in vol.1 layer 0.75 oz glass,+/−20 deg front+/−45 deg elevator
