Parameter |
Value (US) |
Value (Metric) |
Maximum Gross Takeoff Weight (MGTW) |
27.0 lbs |
12.2 kg |
Nominal Mission Takeoff Weight (NMTW) |
26.2 lbs |
11.88 kg |
Nominal Mission Endurance (MOGAS) |
8-10 hours |
Fuel Type |
Unleaded MOGAS (87 oct. min.) |
Airspeed (Cruise @ NMTW) |
38-50 kts |
70-90 kph |
Airspeed (Dash - level flight @ NMTW) |
55 kts |
102 kph |
Airspeed (Max. Endurance @ NMTW) |
35 kts |
65 kph |
Airspeed (Stall @ NMTW) |
28 kts |
52 kph |
Airspeed (VNE @ NMTW) |
110kts |
203 kph |
Navigation |
DGPS/GPS, DGPS/GPS/INS1 |
Nominal Mission Altitude |
500-1200 ft. AGL |
150-365 meters AGL |
Service Ceiling |
12,000 ft. MSL |
3657 meters MSL |
Launch |
Small Footprint Catapult (<75lbs.) |
Small Footprint Catapult (<34kgs.) |
Recovery |
Belly Skid |
Payload (EO) |
Daylight, RS-170A Std., 10X optical zoom |
Payload (IR) |
320x240, uncooled IR |
Command and Control Radio (C2) |
Up to 2 watt, discrete/frequency agile, Military Band / ISM Band Radio Modem (TX/RX) |
Command and Control Radio Range2 |
20 nm, Line of Sight(LOS) |
36 km, Line of Sight(LOS) |
Video Transmitter |
2 Watt (optional 5W), S-Band FM Video TX with optional 19.2kbps data carrier |
Video Transmission Frequency Range |
S-Band, L-Band |
Video System Range |
20 nm, LOS |
36 km, LOS |
Payload Capacity |
5.0 lbs |
2.2 kgs |
Onboard Power |
BA5590/5390 LiSO2 Battery |
Nominal Mission Fuel Capacity |
90 ounces |
2.6 Liters |
Engine |
1-cylinder (25cc), SOHC, 4-stroke, reciprocating engine with oiling system. |
Ignition |
Electronic, Capacitive Discharge |
Propulsion |
17x8, tractor propeller |
Starting Method |
hand-held electric starter (12V) |
Shipping Size |
60" X 14" X 16" composite box with wheels |
1.52m X 35cm X 40cm composite box with wheels |
Wingspan |
94 inches |
2.4 meters |
Fuselage Length |
58 inches |
1.47 meters |
Tail Height |
11 inches |
28 cm |
Fueslage Diameter |
5 inches |
12.7 cm |
1 - GPS/INS option available Q1, 2006 |
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Note: Air vehicle weights, endurance and link ranges can vary significantly dependant on variant used and mission conditions. Always contact ACR with specific requirements and for further clarification. |
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