Lockheed Martin RQ-3

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AAI RQ-3 DarkStar
Second prototype RQ-3A
Second prototype RQ-3A
Type: Prototype of a reconnaissance drone
Design country:

United StatesUnited States United States

Manufacturer:
First flight:

March 29, 1996

Commissioning:

Flight tests ended in 1999

Production time:

Was never mass-produced

Number of pieces:

2

The Lockheed Martin RQ-3 DarkStar (also known as Tier III-Minus ) is a drone that was created in collaboration between DARPA , Lockheed Martin 's Skunk Works and Boeing on behalf of the Defense Airborne Reconnaissance Office (DARO).

description

The first flight of the RQ-3 took place on March 29, 1996. It was presented to the public on June 1, 1996. This prototype crashed in the same year. A second prototype, the RQ-3A, was completed in 1997 and had its maiden flight in 1998. It has electro-optical sensors and a high-resolution synthetic aperture radar . Due to its stealth properties, the drone is very difficult to detect by enemy radar .

The system can start independently, flies up to 500 miles in its usually heavily protected area of ​​operation, where it can stay for eight hours, and then automatically returns to the base. It is used for tactical reconnaissance and can work with the Global Hawk (Tier II-Plus) reconnaissance aircraft. The program was discontinued in early 1999 for reasons of budget.

During the Iraq war , however, an improved version of the DarkStar is said to have been used. The exact details are secret , but employees of the US Navy and US Air Force have described some features. The airframe should essentially be an enlarged variant of the DarkStar, whereby a lower infrared signature could also be achieved. In the area of ​​avionics, an LPI radar and data link as well as electro-optical sensors are to be used. The data obtained is primarily transmitted via a satellite connection, with the antenna on the top of the machine to protect it from hostile SIGINT sensors. The drones were only produced in very small numbers and never went into series production.

Technical specifications

RQ-3 Dark Star at the Dryden Flight Research Center on Edwards AFB in California
Parameter Data
crew no
length 4.57 m
span 21.03 m
height 1.06 m
Empty mass 1980 kg
Max. Takeoff mass 3855 kg
Top speed 460 km / h
Service ceiling approx. 13,500 m
Use radius 925 km
Max. Duration of use more than 8 h
Engine a Williams-Rolls FJ44-1A turbofan engine with approx. 8.5 kN thrust
Armament no

Trivia

Web links

Commons : RQ-3 Dark Star  - Album with pictures, videos and audio files

Individual evidence

  1. AviationWeek - A Classified Lockheed Martin Unmanned Reconnaissance Aircraft Was Used in Iraq  ( Page no longer available , search in web archivesInfo: The link was automatically marked as defective. Please check the link according to the instructions and then remove this notice. , July 6, 2003@1@ 2Template: Dead Link / www.aviationweek.com