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Northrop Grumman RQ-8A Fire Scout
Photo: Daderot · Wikimedia Commons · CC0
REC // INTEL FEED

NorthropGrummanRQ-8AFireScout

Utility / Transport Helicopters · United States · 2000
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NorthropGrummanRQ-8AFireScout

Northrop Grumman RQ-8A Fire Scout
Northrop Grumman RQ-8A Fire Scout Photo: Daderot · Wikimedia Commons · CC0
* Absolute score — assessed within category · no era adjustment
Payload / Capacity
40
Range
35
Versatility
55
Reliability
50
Speed
45
Survivability
30
Hot-and-High Performance
40
Maintainability
60
Technology
70
Cost-Effectiveness
55
Origin United States
ManufacturerLockheed Martin, L3 Technologies, Sierra Nevada Corporation, Schweizer Aircraft Corporation, Israel Aerospace Industries TAMAM Division, Northrop Grumman Electronic Systems, Teledyne Ryan
CategoryUtility / Transport Helicopters
EraPost-Cold War
In service2000–2022
Operators2 countries
Quantity30
Data Quality83%
46
Utility / Transport Helicopters MASS Rating
26/28
Post-Cold War
162/208
All-Time
Utility / Transport Helicopters · 10 axes scored
Payload / Capacity
40
Range
35
Versatility
55
Reliability
50
Speed
45
Survivability
30
Hot-and-High Performance
40
Maintainability
60
Technology
70
Cost-Effectiveness
55
ⓘ Regardless of era, the same scoring system applies to all units in the utility / transport helicopters category.
01 / Overview
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
UTILITY / TRANSPORT HELICOPTERS · POST-COLD WAR
26
PERFORMANCE/PRICE
65
UNIT COST (2025 USD)
—
46
utility / transport helicopters category
ⓘ Performance/Price and MASS score are computed across all units in the utility / transport helicopters category, regardless of era.
02 / Specs & Design
◎General6MOD.6
  • First Flight2000
  • Service Entry Year2009
  • Crew0
  • Passengers0
  • Primary Rolereconnaissance, situational awareness, aerial fire support and precision targeting support
  • In ServiceNo
◈Powerplant8MOD.8
  • Engine Typeturboshaft
  • Number of Engines1
  • Engine Power (each)313 kW
  • Transmission Rating313 kW
  • Rotor Configurationsingle main rotor
  • Main Rotor Diameter8.38 m
  • Main Rotor Blades3
  • Anti-Torque Typetail rotor
▣Performance10MOD.10
  • Top Speed217 km/h
  • Cruise Speed195 km/h
  • Never-Exceed Speed (VNE)232 km/h
  • Service Ceiling6,100 m
  • Hover Ceiling (IGE)4,572 m
  • Hover Ceiling (OGE)3,048 m
  • Range200 km
  • Ferry Range550 km
  • Rate of Climb8.5 m/s
  • Endurance180
◇Dimensions & Weights7MOD.7
  • Fuselage Length7.3 m
  • Height2.96 m
  • Rotor Disc Area55.1
  • Empty Weight626 kg
  • Max Takeoff Weight1,433 kg
  • Useful Load807 kg
  • Cabin Volume0
◆Armament & Mission3MOD.3
  • Hardpoints0
  • Weapons Payload90 kg
  • Gunnone
▲Production2MOD.2
  • Total Built30
  • Variants1
◎Service History4MOD.4
  • Retirement Year2022
  • Production Start2000
  • Production End2022
  • Operational Statusretired
03 / History
SERVICE LIFESPANStill in Service
  1. 2000Production started
  2. 2022Production ended
26
years in service
22
years in production
30
units produced
2
countries operating
ⓘ The producing country still actively operates it.
04 / Operators
Operator Countries2country
📖 TERMS ON THIS PAGE3terms
Autopilot/AFCS (Automatic Flight Control System) is an avionics suite that automatically controls a helicopter’s attitude, navigation and flight path, providing stability augmentation and reducing pilot workload.
Combined forward-looking infrared (FLIR) and electro-optical (EO) sensor turret for target acquisition and tracking, typically mounted on aircraft or ground vehicles.
A sight mounted on a helicopter's mast for targeting.
These terms are listed automatically because they appear on this page.full encyclopedia →
📚 Sources
📖 ENCYCLOPEDIA Browse the Utility / Transport Helicopters entry →