Orbiter
Initial Operational Capability (IOC) : 2006
Total Production : ?
Model | Status | Year | Produced |
---|---|---|---|
Orbiter | Active | 2006 | ? |
Orbiter
Group : mini-UAVs
Status : Active
Origin : Israel
Contractor : Aeronautics Defense Systems
Initial Operational Capability (IOC) : 2006
Total Production : ?
The Orbiter is a day/night, compact, lightweight, tail-less Mini Unmanned Aerial Vehicle (MUAV) developed by Aeronautics Defense Systems to perform homeland security and tactical military missions. The system represents the ultimate solution for Over The Hill reconnaissance missions, Low Intensity Conflicts and Urban warfare operations as well as any close range Intelligence, Surveillance and Reconnaissance (ISR) mission. It has been designed to fly missions of 2.5 to 3 hours at ranges of up to 40 kilometers using a mini ground directional antenna. A single Orbiter system consists of a two-man crew, launch and control equipment and an air vehicle fitting into one backpack.
The Orbiter is powered by an electric motor and is designed for use by a single operator. It features autonomous launch and recovery modes using a catapult and a parachute respectively. It can fly both operator directed via a line-of-sight data link or pre-programmed flight paths. The air vehicle is equipped with advanced avionics, state-of-the-art payloads, advanced data link system, and an accurate navigation system combining GPS and INS. Its electric motor provides a low acoustic signature which enhances the survivability on the theater of operations while flying between 500-to-2,000-ft (150-to-700 meters) of altitude. Each Orbiter system includes three air vehicles.
Operators
Country | Status | State | Notes |
---|---|---|---|
![]() | Active | ? | |
![]() | Active | ? | Azerbaijan ordered 60 Orbiter and Aerostar UAVs in 2011 |
![]() | Active | ? | |
![]() | Active | ? | Not confirmed, sold in May 2008? |
![]() | Active | ? | |
![]() | Active | ? | |
![]() | Active | 18 | Six systems with three air vehicles each |
![]() | Active | ? |
Specifications
Notes | ||
---|---|---|
Crew | 0 | |
System Crew | 2 | |
Dimensions | ||
Height | 0.30 meter | |
Length | 1 meter | |
Wingspan | 2.2 meter | |
Mass | ||
Max Takeoff Weight | 6.5 kilogram | |
Payload | 1.5 kilogram | |
Performance | ||
Ceiling | 18,000 foot | |
Operational Altitude | 2,000 foot | |
Radius of Operation | 40 kilometer | using ground directional antenna or 15 km using line-of-sight data link |
Speed | ||
Cruise Speed | 65 knot | |
Top Speed at High Altitude | 75 knot | |
Time | ||
Flight Endurance | 3 hour |
News
Hunt Valley, Maryland — May 14, 2009 — AAI Corporation, an operating unit of Textron Systems, a Textron Inc.
Hunt Valley, Maryland — February 24, 2009 — AAI Corporation, an operating unit of Textron Systems, a Textron Inc.
Hunt Valley, Maryland and Yayne, Israel — September 29, 2008 — AAI Corporation, an operating unit of Textron Systems, a Textron Inc.

The Orbiter™ Mini UAV has successfully completed a series of flights in a live-fire artillery exercise in Southern Israel.
Aeronautics Defense Systems Ltd. signs $3 m contract to supply six Orbiter mini UAV systems to the Polish Army.
Photo Gallery
Notes
State Latest Known holdings/Original Procurement
Com - Date of Commissioning
Decom - Date of Decommissioning
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