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SUPAPUP Light Aircraft

http://users.senet.com.au/~supapup/index.html

Supapup MK 4

Take off: 200 meters to clear 50 feet (40 hp) Cabin width at shoulders: 584 mm (24") Bubbled windows can extend this to 28"

Height seat to roof skylight 940mm (37") Plenty of room for a long legged 6'4" Pilot Rudder pedals are adjustable

DIMENSIONS	.	SPECIFICATIONS	UL           VH	IMP
Length	5.7 M	Empty Wt : Depd on access	180 to 200 Kg	397 to 440 Lb
Wing Span	7.925 M	Max T.O. Weight	340 Kg	750 Lb
Wing Area	9.5 Sq M	Fuel Cap (in wings)	54 Lt	14 US Gal.
Aspect Ratio	6.5	VNE Vehicle never exceed	200 Kmh	130 Knots
Wing Chord	1.225 M	Cruise Airspeed	185 Kmph	100 Knots
Dihedral	2 Deg	Stall Airspeed	66 Kmph	35 Knots

ENGINES	TYPE	CYLINDER #	POWER	MADE IN
JABIRU     Horizontally opposed	4 Stroke	4 Cylinder	54 Hp	Australia
ROTAX     Vertical Twin, 1 carb.	2 Stroke	2 Cylinder	48 Hp	Austria

*Rate Of Climb (Depending On Prop Type)	.
JABIRU  ROTAX	1100 Fpm   Estm  1100 Fpm   Estm
*Endurance, @75% of max cruise With 10% Reserve	.
JABIRU  ROTAX	4.5 Hrs  w/res 4.5 Hrs  w/res
*Fuel Usage	.
JABIRU  1600 cc ROTAX   503 Dual Ign CDI	10    Lt/Hr 10    Lt/Hr

* Mathematical projections based on manufactures specifications and flight tests