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A2C2S

A2C2S

Utility & Transport Helicopters
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Basic Information
Name
A2C2S
Designation
A2C2S
Alternate Designation
C2 on-the-move
Equipment Type
Utility & Transport Helicopters
Manufacturer
Raytheon, Sikorsky Aircraft Corporation
Date of Introduction
2004
Description

The Army Airborne Command and Control System (A2C2S) is a derivative of proven UH-60L helicopter carrying a dedicated mission equipment package to provide US Army's brigade, divisions and corps commanders with an airborne command post with continuous situational awareness, robust communications and over-the-battlefield mobility. The A2C2S system features non-line-of-sight radios, wide band digital radios and six workstations. The US Army shows regard for the A2C2S as an element of the future Objective Force. After more than 3,000 operational hours, 2,000 of them in combat, meeting and exceeding performance and reliability requirements the first low rate initial production (LRIP) A2C2S was delivered to the US Army on December 16, 2004. Raytheon is under contract to provide five LRIP systems and two A-kits for EUH-60 helicopters. Additional orders are anticipated in fiscal year 2005. Also dubbed 'C2 on-the-move', this airborne platform operates through the battlespace at 120 miles per hour (180 km/h). The US Army plans call for approximately 120 systems to be fielded during the life of the program. On 1 March 2005, Raytheon aired that the A2C2S had demonstrated well suited for homeland defense during exercises simulating Huntsville's 1989 tornado conducted by the US Army National Guard. As of March 20005, A2C2S had logged more than 2,000 hours of operations in support of combat and peacekeeping missions in the Middle East.

Air & Air Defense Specifications
Crew 4
Max Speed 360.0 km/h
Range 567.0 km
Service Ceiling 5837 m
Overview (Deagel)
Group Utility & Transport Helicopters
Status Cancelled
Also Known As C2 on-the-move
Origin United States of America
Contractors Raytheon*, Sikorsky Aircraft Corporation
Initial Operational Capability (IOC) 2004
Total Production 120
Specifications (Deagel)
Crew 4
Main Rotor Blades 4
Number of Engines 2
Troops 6
Dimensions — Height 5.1 meter
Dimensions — Length 1,976 meter
Dimensions — Main Rotor Diameter 16.4 meter
Dimensions — Width 2.4 meter
Mass — Empty Weight 5,919 kilogram
Mass — Max Takeoff Weight 10,660 kilogram
Performance — Ceiling 5,837 meter
Performance — Max Range 567 kilometer
Power — Max Power at TakeOff 3,780 shp
Speed — Cruise Speed 77.2 mps
Speed — Top Speed at High Altitude 100 mps
Time — Flight Endurance 2.1 hour
Gear (Deagel)
Item 1 Turboshaft Engines: T700-GE-701C (2)
Variants
Variant 1 UH-60A Blackhawk
Variant 2 HH-60G Pave Hawk
Variant 3 SH-60B Seahawk
Variant 4 SH-60F Ocean Hawk
Variant 5 UH-60L Blackhawk
Variant 6 HH-60H
Variant 7 UH-60Q Medevac
Variant 8 MH-60S Knighthawk
Variant 9 A2C2S
Variant 10 MH-60R Strikehawk
Variant 11 HH-60M BlackHawk
Variant 12 UH-60M BlackHawk
Variant 13 BattleHawk
Variant 14 MH-60M BlackHawk
Variant 15 Advanced UH-60J
Variant 16 S-70i International Black Hawk
Variant 17 UH-60V Blackhawk
Variant 18 HH-60W Jolly Green II
Details
Country of Origin United States
Category Transport Helicopter
Air > Transport Helicopter
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
Width
2.4 m
Height
5.1 m
Weight
10660 kg
Operators (1)
United States
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