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RQ-8A Fire Scout

RQ-8A Fire Scout

Reconnaissance Rotorcrafts
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Basic Information
Name
RQ-8A Fire Scout
Designation
RQ-8A Fire Scout
Alternate Designation
MQ-8
Equipment Type
Reconnaissance Rotorcrafts
Manufacturer
Northrop Grumman, Schweizer Aircraft
Date of Introduction
2005
Description

The RQ-8A Fire Scout also includes a HMMWV-mounted ground control station for use by the USMC and the the Tactical Control Station (TCS) developed for US Navy ships. It provides coverage 110nm from launch site providing ISR (Intelligence Surveillance and Reconnaissance) and targeting through its Electro-Optical and IR sensors and a laser designator. The Fire Scout will also act as a communications node within the network centric warfare battle space supporting other platforms. It is powered by a single Rolls Royce 250-C20W engine and features a 3-blade main rotor that could be replaced by a 4-blade rotor extending Fire Scout range, payload and flight endurance. The Fire Scout will replace the Pioneer UAV. In the future, the valuable Fire Scout will provide accurate targeting to warships equipped with Extended Range Guided Projectiles (ERGM) and land attack missiles. For this reason the US Army and the US Navy are testing the Fire Scout under the MQ-8 designation. In 2005 the RQ-8 program was restructured with the RQ-8A aircraft deemed as the test version of more capable MQ-8B which was scheduled to be the first full operational model deployed with the Armed Forces of the United States.

Air & Air Defense Specifications
Crew 0
Max Speed 234.0 km/h
Range 204.0 km
Service Ceiling 6100 m
Overview (Deagel)
Group Reconnaissance Rotorcrafts
Status Cancelled
Also Known As MQ-8
Origin United States of America
Contractors Northrop Grumman*, Schweizer Aircraft
Initial Operational Capability (IOC) 2005
Total Production ?
Specifications (Deagel)
Crew 0
Main Rotor Blades 3
Number of Engines 1
Dimensions — Height 2.9 meter
Dimensions — Length 7.0 meter
Mass — Max Takeoff Weight 1,157 kilogram
Performance — Ceiling 6,100 meter
Performance — Max Range 204 kilometer
Speed — Top Speed at High Altitude 65 mps
Time — Flight Endurance 6 hour
Gear (Deagel)
Item 1 Turboshaft Engines: Model 250-C20W (1)
Variants
Variant 1 RQ-8A Fire Scout
Variant 2 MQ-8B Fire Scout
Variant 3 MQ-8C Fire Scout
Details
Country of Origin United States
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
7 m
Width
Height
2.9 m
Weight
1157 kg
Related Equipment (1)
Operators (1)
United States
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