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UCAR

UCAR

Attack Helicopters
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Basic Information
Name
UCAR
Designation
UCAR
Alternate Designation
Equipment Type
Attack Helicopters
Manufacturer
Lockheed Martin, Northrop Grumman, Textron
Date of Introduction
2015
Description

The Unmanned Combat Armed Rotorcraft (UCAR) is being designed to perform attack and reconnaissance missions in support of the FCS unit of action. The UCAR would be controlled remotely by the RAH-66 Comanche helicopter, the A2C2S helicopter and ground control stations. In 2004 RAH-66 Comanche manned attack helicopter was cancelled favoring Apache improved models and UCAR development. It will operate at low altitude jointly with manned and unmanned aircraft with critical decisions such as open fire against a potential targets taken by human operators. Currently, the UCAR program is being managed by DARPA and the US Army under feasibility studies. Two teams lead by Northrop-Grumman and Lockheed-Martin are the bidders for this program. The Critical Design Review of the project is scheduled for April 2005 as part of the program's Phase III effort. The US Army plans to field a first operational UCAR aircraft by 2015. The US Army intends to field a rotary wing unmanned combat vehicle capable of performing with awesome vertical lift and speed skills. Current figures suggest that the UCAR would be able to climb at 500-ft per minute (152 meters/minute) reaching a ceiling altitude of 18,600-ft (+5,600 meters). Moreover, the UCAR would fly at a maximum speed of 170 knots (+300 kph) with a gross weight of 5,500 pounds (2,500 kg). The US Army has high demanding requirements for hot-day performance (for example 95 degree Farenheit) consisting of 6,000-ft (+1,800 meters) ceiling altitude while retaining a 500-ft per minute climb rate.

Air & Air Defense Specifications
Max Speed 314.8 km/h
Service Ceiling 5669 m
Overview (Deagel)
Group Attack Helicopters
Status Under Development
Origin United States of America
Contractors Lockheed Martin, Northrop Grumman, Textron
Initial Operational Capability (IOC) 2015
Total Production ?
Specifications (Deagel)
Crew 0
Mass — Max Takeoff Weight 5,500 pound
Performance — Ceiling 18,600 foot
Speed — Top Speed at High Altitude 170 knot
Gear (Deagel)
Item 1 Attack Helicopters: RAH-66 Comanche
Item 2 Utility & Transport Helicopters: A2C2S
Details
Country of Origin United States
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
Width
Height
Weight
2494.76 kg
Operators (1)
United States
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