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MQ-8B Fire Scout

MQ-8B Fire Scout

Reconnaissance Rotorcrafts
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Basic Information
Name
MQ-8B Fire Scout
Designation
MQ-8B Fire Scout
Alternate Designation
Class IV UAS, RQ-8B Fire Scout
Equipment Type
Reconnaissance Rotorcrafts
Manufacturer
Northrop Grumman, Schweizer Aircraft
Date of Introduction
2008
Description

In early 2004 the FCS lead systems integrators, Boeing and SAIC, selected Northrop-Grumman RQ-8B Fire Scout as the FCS Class IV Unmanned Aerial System (UAS). The FCS Class IV UAS will perform Intelligence, Surveillance, Reconnaissance, Targeting and Precision Strike missions. The RQ-8B UAS will feature a new four-blade rotor, versus the three-blade rotor of A models, that will provide better flight characteristics and the capability to accommodate greater payloads. The flight endurance carrying a 130-pound (59 kg) payload will exceed eight hours. The maximum payload capacity could reach the 600-pound figure. The weapon options related to the Class IV UAS will include laser guided APKWS rockets and Viper Strike precision munitions. The electronic package, ground control station, sensors and other equipment must be selected by FCS lead systems integrators. Typically, the Class IV UAS (Fire Scout) will operate at 150 nautical miles from its ground station carrying a wide range of payloads depending on the mission requirement. In 2005, the RQ-8B was re-designated as the MQ-8B Fire Scout to reflect its multi-mission capabilities which included the ability to fire weapons in addition to the Intelligence, Surveillance and Reconnaissance (ISR) capabilities demonstrated on the RQ-8A model. The US Navy slated the MQ-8B UAV to be fielded with the Littoral Combat Ship (LCS) beginning in 2009. As of early 2006, Northrop-Grumman was producing 12 MQ-8B Fire Scout aircraft. Four for the US Navy and eight for the US Army. In August 2006, the US Navy awarded Northrop-Grumman a $136 million modification contract to complete the Vertical Take-off and Landing Tactical Unmanned Air Vehicle (VTUAV) System Development and Demonstration (SDD) phase through 2008. A total of nine MQ-8B Navy Fire Scouts are planned to be built under the SDD phase. In February 2007, the US Navy ordered two more aircraft. The program was cancelled in favor of the larger MQ-8C.

Air & Air Defense Specifications
Crew 0
Max Speed 234.0 km/h
Range 280.0 km
Service Ceiling 6100 m
Overview (Deagel)
Group Reconnaissance Rotorcrafts
Status Cancelled
Also Known As Class IV UAS, RQ-8B Fire Scout
Origin United States of America
Contractors Northrop Grumman*, Schweizer Aircraft
Initial Operational Capability (IOC) 2008
First Flight December 2006
Total Production 175
Unitary Cost USD $16.2 million
Specifications (Deagel)
Crew 0
Main Rotor Blades 4
Number of Engines 1
Dimensions — Height 2.9 meter
Dimensions — Length 7.0 meter
Mass — Payload 272 kilogram
Performance — Ceiling 6,100 meter
Performance — Max Range 280 kilometer
Speed — Top Speed at High Altitude 65 mps
Time — Flight Endurance 8 hour
Gear (Deagel)
Item 1 Anti-Tank Glider Weapons: GBU-44/B Viper Strike (2)
Item 2 Mapping Systems: AACER (1)
Item 3 Optronic Systems: AN/DVS-1 COBRA (1)
Item 4 Optronic Systems: ASTAMIDS (1)
Item 5 Optronic Systems: Brite Star II (1)
Item 6 Radar Systems: RDR-1700B+ (1)
Item 7 Rockets: APKWS (8)
Item 8 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
Related Equipment (1)
Operators (1)
United States
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