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Panther

Panther

Reconnaissance Rotorcrafts
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Basic Information
Name
Panther
Designation
Panther
Alternate Designation
Equipment Type
Reconnaissance Rotorcrafts
Manufacturer
Israel Aerospace Industries Ltd. (IAI)
Date of Introduction
2011
Description

The Panther is a tilt-rotor unmanned aerial vehicle (UAV) designed by IAI to conduct Intelligence, Surveillance and Reconnaissance (ISR) missions from unprepared areas. The Panther combines the flight capabilities of an airplane with helicopter-like hovering. The airframe consists of three tilt-rotor propellers and a fixed wing vertical takeoff and landing (VTOL) system, which enable a runway-free takeoff and landing on an unprepared area. This UAV layout has been patented by IAI. The Panther was unveiled in early October 2010 after having completed a series of flight tests using prototypes. The UAV system is expected to go operational with the Israel Defense Forces by 2011. It can take off and land automatically by a simple click of the operator console, thus eliminating the need for an external pilot. The automatic flight control system controls the transitions between the hovering takeoff phase to forward flight and vice versa before landing. The three propellers are driven by three independent ultra-quiet electric motors. The air vehicle weighs 65 kg and can loiter for approximately six hours with a radius of operation of 60 kilometers and an altitude of 10,000-ft. It carries a MiniPOP payload fitted with day/night stabilized camera with a laser range finder, pointer or laser designator. The Mini Panther is a man-portable smaller version weighing up to 12 kg that can loiter for approximately 2 hours, carrying a Micro-POP payload. The Panther control station, transported on a midsize vehicle, can store up to three aircraft, as well as the ground data link, the support equipment and spare parts, all of which allow the troops' autonomous operation on the field at a tactical level. Two operators control the mission using two fully redundant identical consoles. The Mini Panther system includes two air vehicles and a command and control unit, and is carried in backpacks by two soldiers. Designed to be entirely automatic, both Panther and Mini Panther can be controlled by one operator, while the command and control station has two operators to control the station and oversee the mission.

Air & Air Defense Specifications
Range 60.0 km
Service Ceiling 3048 m
Overview (Deagel)
Group Reconnaissance Rotorcrafts
Status Under Development
Origin Israel
Contractor Israel Aerospace Industries Ltd. (IAI)
Initial Operational Capability (IOC) 2011
First Flight 2010
Total Production ?
Specifications (Deagel)
Crew 0
Number of Engines 3
System Crew 2
Mass — Max Takeoff Weight 65 kilogram
Performance — Ceiling 10,000 foot
Performance — Radius of Operation 60 kilometer
Time — Flight Endurance 6 hour
Gear (Deagel)
Item 1 Optronic Systems: MiniPOP (1)
Details
Country of Origin Israel
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
Width
Height
Weight
65 kg
Operators (1)
Israel
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