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Manta B Specifications
| Parameter |
Value (U.S.) |
Value (Metric) |
Maximum Gross Takeoff Weight (MGTW) |
52 lbs
|
23.5 kg
|
Nominal Mission Takeoff Weight (NMTW) |
45 lbs
|
20.4 kg
|
Nominal Mission Endurance (87 octane gasoline) |
6+ Hours
|
Fuel Type |
50:1 Gasoline/Oil Pre-Mix
|
Airspeed (Cruise @ NMTW) |
39 - 70 knots
|
72 - 130 kph
|
Airspeed (Dash - Level Flight @ NMTW) |
70 knots
|
130 kph
|
Airspeed (Max. Endurance @ NMTW) |
39 knots
|
72 kph
|
Airspeed (Stall @ NMTW) |
35 knots
|
64 kph
|
Airspeed (VNE @ NMTW) |
110 knots
|
203 kph
|
Navigation |
DGPS/GPS, DGPS/GPS/INS1
|
Service Ceiling |
16,000 feet MSL
|
4,870 meters
|
Launch |
Wheeled, Vehicle Based, or Launcher (Coming Soon)
|
Recovery |
Parachute or Gear
|
Payload (EO) |
PTZ Daylight Camera
|
Payload (IR) |
PTZ IR camera
|
Command and Control Radio (C2) |
Up to 2 Watt, Discrete/Frequency Agile,
Military Band / ISM Band Radio Modem (TX/RX)
|
Command and Control Radio Range |
15-20 nm, Line of Sight (LOS)
|
24-32 km, Line of Sight (LOS)
|
Video Transmitter |
2 Watt (Optional 5W), S-Band FM Video TX
With Optional 19.2kbps Data Carrier
|
Video System Range |
15-20 nm, LOS |
24-32 km, LOS |
Payload Capacity |
Up To 15.0 lbs |
Up To 6.8 kg |
Onboard Power |
BA5590 LiSO2 Battery
(One or two batteries can be installed)
|
Onboard Power Capacity |
14.4V, 15 or 30 AH
|
Nominal Mission Fuel Capacity |
1.9 Gallons
|
7.2 Liters
|
Engine |
2-Stroke Reciprocating Gasoline Engine (87 Octane)
Reverse Rotation
|
Ignition |
Electronic, Capacitive Discharge
|
Propulsion |
18x12, Tractor Propeller
(In Reverse Rotation)
|
Starting Method |
Hand-Held Electric Starter (12V)
|
Shipping Container Size |
49" x 52" x 24"
|
1.24m x 1.3m x 0.61m
|
1 - GPS/INS option available Q1, 2006
Manta B Specifications .pdf
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3292 East Hemisphere Loop • Tucson, Arizona 85706
T: 520.573.6300 • F: 520.573.2057 • www.acrtucson.com |
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