General Specifications
Powerplant	Modified AirResearch JFS-100-13A
Horsepower	100
Seats	2
Gross Weight	1,250 lbs (567 kg)
Empty Weight	675 lbs (306 kg)*
Fuel Capacity	20 gal (76 liters)
Useful Load	575 lbs (261 kg)*
Performance (Est.)
Hover IGE (5' skid ht)	8,000' (2,438 m)
Hover OGE	4,000' (1,219 m)
Service Ceiling	10,000' (3,048 m)
Cruise Range (10% reser.), SL	123 miles (198 km)
Normal Cruise Speed, SL	81 mph (70 kts)
Max Speed, SL	108 mph (94 kts)*
Basic Dimensions
Main Rotor Diameter	23' (7.01 m)
Tail Rotor Diameter	2.6' (0.79 m)
Overall Length (nose-to-tail)	19' (5.79 m)
Cabin Width	4.1' (1.24 m)
Skid Width	5.5' (1.68 m)
Height	7.8' (2.51 m)

* with carbon fiber fuselage

EFFECT OF ALTITUDE ON HX-2 WASP PERFORMANCE
CONDITIONS
	ROTOR SPEED= 500 rpm
	FUEL WEIGHT= 140 lbs
	EMPTY WEIGHT= 675 lbs
	NO RESERVE FUEL
CASES
	GR. WEIGHT	MAX. POWER	ALTITUDE
I	1,250 lbs	110 hp	SL
II	1,250 lbs	87 hp	6,200 ft
III	1,020 lbs	87 hp	6,200 ft
CASES	HOVER, OGE	VMIN, mph	ENDURANCE, hrs	RANGE, miles	VMAX, mph	USEFUL LOAD, lbs
I	Y	0	1.98	137	108	575
II	N	32	2.06	154	89	575
III	Y	0	3.07	211	106	345