Illustration of the NightHawk QS3 in camouflage flying low over a coastal city

Specifications

Speed & Endurance

Speed:

knots max cruise
–93 knots loiter

Endurance:

hours loiter
+ hours w/ external aux tanks
> hours loiter as UAV

Range:

> NM w/ external wing tanks
+ NM @ 130 knots as UAV

NightHawk QS3

Long Endurance ISR Platform with Low Acoustic and Low Thermal Signatures

The NightHawk is a long endurance ISR platform with low acoustic and low thermal signatures, that is capable of manned and unmanned operations. Its advanced aerodynamic design, high efficiency turbo-diesel engine and carbon fiber construction enable a range of up to 5000 NM at cruise or approximately 60 hours of endurance while loitering, with a payload of 500 pounds operating as a UAV. The NightHawk also provides over 135 ft³ of internal space for payload and cargo. Designed to be rapidly deployable via a C-17, its outer wing panels can be removed in less than 30 minutes by two individuals. There are two (2) hardpoints, designed to carry 450-pound loads on the wings which can be used to carry external sensors and/or auxiliary fuel. The NightHawk is currently TRL 8 as a manned aircraft and TRL 3 as a UAS.

Top-view diagram of the NightHawk QS3: two fuel tanks per wing (35-gallon main, 24-gallon auxiliary; 118 gallons total), wings removable in 15 minutes to fit a C-17, and fiberglass wingtips and vertical tip used as antenna locations
Top-view diagram of the NightHawk QS3: approximately 110 cubic-foot cabin (135 cubic feet total internal space) over 15 feet long with three tandem seats, dual flight controls, autopilot and Garmin G3X Touch displays; turbocharged 260 hp SMA/Röder aerodiesel with a maximum cruise of 165 knots and about 4 gallons per hour at loiter (85 to 93 knots); concealed PBS TJ-100 turbojet backup of about 300 lbf, estimated 100 knots

Base Specifications

Wingspan57’ 4” (17’ without outer wing panels)
WeightMaximum gross weight – 4500 pounds, empty 2350 pounds
Height11’, 2”
Length29’
Engine (primary)SAFRAN SR305-260E, 260 HP
Engine (backup)PBS TJ-100 turbojet, 300 pounds thrust, stored w/in fuselage tail cone
FuelsJP-8, Jet A, Jet A-1
Fuel Tanks118-gallon wing tank
Aux fuel tanksTwo 30-gallon externally mounted wing tanks
SpeedMaximum cruise 165 knots
Range>3000 NM with two 30-gallon external wing tanks
Endurance25 hours loiter time (40+ hours w/external auxiliary tanks)
Ceiling> 26,000′ MSL (expecting 30,000′)
Sensor Payload18 ft³ in primary sensor bay, plus four locations throughout aircraft for concealed or enclosed equipment
Cabin ConfigurationManned ISR configuration – three stations: pilot, copilot/sensor operator and
additional sensor operator/crew.
Utility configuration – 1 crew & space for 4 pax or 1000 pounds of cargo (~110 ft³)

UAV Configuration

MTOW4500 pounds (with operating limitations)
Internal fuel capacity250 gallons total (118-gallon wing tank, 132-gallon internal aux tank)
Range5000+ NM @ 130 knots
Endurance>60 hours loiter time
Payload>400 pounds with full load of fuel and 160 ft³ of concealed/internal space

Manned ISR Configuration

CrewUp to three – pilot, copilot (and/or sensor operator) and sensor operator
Sensor bay18 ft³ primary sensor bay plus four locations throughout aircraft for concealed or enclosed equipment

*Note – Specifications will vary by configuration, intended use, sensor options and mission parameters.