Aircraft
Training Aircraft
The school has assembled a unique and diverse fleet of 28 aircraft with 16 jet trainers, three transonic fighters, a seaplane and several helicopters. Training types include the Hawker Hunter T.7, Aero Vodochody L-39 and L-29, Bombardier Challenger, Embraer Phenom, as well as MBB Bo 105M and Bell 206B3 helicopters, among others.
The L-39 Albatros fleet has been upgraded with full-colour touchscreen displays and hands on throttle and stick (HOTAS) controls. Simulation is heavily incorporated into all training programs, and the school employs virtual reality (VR) and mixed reality (MR) to boost training effectiveness.
Simulators
ITPS puts the emphasis on technology. The school employs modern avionics, head-up display (HUD) technology, tactical datalink, live virtual constructive training (LVCT) and advanced simulation systems to enhance its flight test training programs. Simulators – including F-16C, F/A-18E, F-35, Boeing 787, AH-64D/E and AW139 units – are used throughout the test pilot and flight test engineer training programmes.
They facilitate instruction in electronic flight information and HUD systems evaluation, fly-by-wire flight control laws, autopilot and flight management systems assessment. ITPS has also contracted with CAE’s Toronto training centre to access a number of full-motion commercial aircraft simulators for test pilot school exercises.
Fleets
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Hawker Hunter T.7
The Hawker Hunter T.7A (5STA) is a British two-seat jet trainer aircraft developed from the single-seat Hunter fighter. Operated as a 5th Generation Surrogate Training Aircraft, the 5STA modification is upgraded with modern avionics, data link systems, and threat simulation capabilities to support advanced pilot training. Its performance and handling qualities make it ideal for replicating aspects of 5th generation combat aircraft operations in a cost-effective platform.
General Characteristics
- Crew: two
- Length: 45 ft 10 in (13.97 m)
- Wingspan: 33 ft 8 in (10.26 m)
- Height: 13 ft 2 in (4.01 m)
- Empty weight: ~14,000 lb (6,350 kg)
- Gross weight: ~24,000 lb (10,886 kg)
- Fuel capacity: Internal tanks with approximately 600 imperial gallons (2,730 liters); optional external tanks
- Powerplant: 1 × Rolls-Royce Avon 100-series turbojet engine, 10,150 lbf (45.2 kN) thrust
Performance
- Maximum speed: 620 kn (715 mph, 1,150 km/h) at altitude
- Cruise speed: ~485 kn (558 mph, 898 km/h)
- Range: ~1,850 nmi (2,130 mi, 3,430 km) with external tanks
- Service ceiling: 50,000 ft (15,240 m)
- Rate of climb: ~15,000 ft/min (76.2 m/s)
Avionics (5STA Upgrade)
- Glass cockpit with modern multifunction displays (MFDs)
- Hands-On Throttle and Stick (HOTAS)
- Embedded simulation and threat replicator suite
- Tactical data link
- GPS/INS navigation system
- Electronic warfare training suite
- Secure comms and dual UHF/VHF radios
- Radar warning receiver and countermeasure dispenser (training simulation only)
AERO Vodochody L-39 Albatros
The Aero L-39 Albatros is a Czech subsonic jet trainer aircraft, developed by Aero Vodochody. Designed for basic and advanced pilot training, the L-39 features a tandem cockpit, rugged tricycle landing gear, and a single turbofan engine. Some L39 aircraft operated by ITPS (Canada) Ltd. have been upgraded with modern avionics/AUPs to support 4th and 5th gen training.
General characteristics
- Crew: two
- Length: 39 ft 11 in (12.13 m)
- Wingspan: 31 ft 0 in (9.46 m)
- Height: 15 ft 6 in (4.72 m)
- Empty weight: 7,495 lb (3,400 kg)
- Gross weight: 10,360 lb (4,700 kg)
- Fuel capacity: approx. 394 US gallons (1,490 liters) internal; optional external drop tanks
- Powerplant: 1 × Ivchenko AI-25TL turbofan, 3,790 lbf (16.9 kN) thrust
Performance
- Maximum speed: 470 mph (750 km/h, 405 kn) at altitude
- Cruise speed: 362 mph (583 km/h, 315 kn)
- Range: 590 nmi (680 mi, 1,100 km) with internal fuel
- Service ceiling: 36,000 ft (11,000 m)
- Rate of climb: 4,330 ft/min (22 m/s)
Avionics (Upgraded ITPS Aircraft)
- Glass cockpit with multifunction displays (MFDs)
- Head-Up Display (HUD) and HUD repeater
- Embedded GPS navigation
- Mission replay and debriefing system
- UHF/VHF communications radios
AERO Vodochody L-29 Delfin
The Aero L-29 Delfín is a Czech subsonic jet trainer developed by Aero Vodochody in the late 1950s. As the standard jet trainer for Warsaw Pact nations, the L-29 is known for its simplicity, rugged construction, and forgiving handling characteristics. It remains in use today in civilian training, warbird, and heritage flight roles. A small number are still operated in flight test support and advanced pilot training environments.
General characteristics
- Crew: two
- Length: 35 ft 6 in (10.81 m)
- Wingspan: 34 ft 5 in (10.46 m)
- Height: 12 ft 5 in (3.77 m)
- Empty weight: 5,291 lb (2,400 kg)
- Gross weight: 7,937 lb (3,600 kg)
- Fuel capacity: approx. 300 US gallons (1,135 liters) internal
- Powerplant: 1 × Motorlet M-701C turbojet, 1,985 lbf (8.8 kN) thrust
Performance
- Maximum speed: 407 mph (655 km/h, 354 kn) at altitude
- Cruise speed: 375 mph (603 km/h, 326 kn)
- Range: 559 nmi (643 mi, 1,035 km) with standard fuel
- Service ceiling: 36,100 ft (11,000 m)
- Rate of climb: 2,755 ft/min (14 m/s)
Sikorsky S-76C+
The Sikorsky S76C+ is an American medium-size commercial utility helicopter, manufactured by the Sikorsky Aircraft Corporation. The S76C+ features twin turboshaft engines, four-bladed main and tail rotors, and retractable landing gear.General characteristics
- Crew: two
- Capacity: 13 passengers
- Length: 52 ft 6 in (16 m) from tip of main rotor to tip of tail rotor
- Width: 10 ft 0 in (3.05 m) at horizontal stabilizer
- Height: 14 ft 6 in (4.42 m) to tip of tail rotor
- Empty weight: 7,005 lb (3,177 kg) in utility configuration
- Gross weight: 11,700 lb (5,306 kg)
- Fuel capacity: 281 US gallons (1,064 liters), with 50 or 102 US gallons (189 or 386 liters) available in extra auxiliary tanks
- Powerplant: Safran Helicopter Engines Arriel 2S1 Turboshaft, 871 Shp (650 kW)
- Main rotor diameter: 44 ft 0 in (13.41 m)
Performance
- Maximum speed: 155 kn (178 mph, 287 km/h) at maximum takeoff weight at sea level in standard atmospheric conditions
- Cruise speed: 155 kn (178 mph, 287 km/h) maximum cruise speed is the same as maximum speed
- Range: 411 nmi (473 mi, 761 km) no reserves, at long-range cruise speed at 4,000 ft altitude
- Service ceiling: 13,800 ft (4,200 m)
MBB Bo105 CDN-BS-4
The MMBB Bo105 CDN-BS-4 is a German light, twin-engine utility helicopter developed by Messerschmitt-Bölkow-Blohm (MBB). Known for its rigid rotor system and excellent agility, the Bo105 was widely used for military liaison, observation, and training roles. It remains in service with several nations and continues to support pilot training and systems evaluation missions.
General characteristics
- Crew: two
- Capacity: 3–4 passengers or mission equipment
- Length: 38 ft 6 in (11.74 m) overall (including rotors)
- Fuselage length: 31 ft 8 in (9.65 m)
- Width: 3 ft 11 in (1.20 m) fuselage
- Height: 9 ft 8 in (2.95 m)
- Empty weight: 2,646 lb (1,200 kg)
- Max takeoff weight: 5,512 lb (2,500 kg)
- Fuel capacity: approx. 156 US gallons (590 litres)
- Powerplant: 2 × Allison 250-C20B turboshaft engines, 420 shp (313 kW) each
- Main rotor diameter: 32 ft 2 in (9.80 m)
- Tail rotor diameter: 3 ft 7 in (1.10 m)
Performance
- Maximum speed: 152 mph (245 km/h, 132 kn)
- Cruise speed: 135 mph (217 km/h, 117 kn)
- Range: 357 nmi (411 mi, 660 km)
- Service ceiling: 17,000 ft (5,180 m)
- Rate of climb: 1,575 ft/min (8.0 m/s)
Bell 206B JetRanger
The Bell 206B JetRanger is a light single-engine utility helicopter developed by Bell Helicopter. Renowned for its simplicity, reliability, and versatility, the JetRanger has been used globally for pilot training, law enforcement, utility work, and flight test support. Its responsive handling and economical operation make it a popular platform for both civilian and military applications.
General characteristics
- Crew: one or two
- Capacity: up to 4 passengers
- Length: 39 ft 8 in (12.09 m) including rotors
- Fuselage length: 31 ft 2 in (9.50 m)
- Height: 9 ft 4 in (2.84 m)
- Empty weight: 2,180 lb (989 kg)
- Max takeoff weight: 3,200 lb (1,451 kg)
- Fuel capacity: approx. 91 US gallons (344 liters)
- Powerplant: 1 × Allison 250-C20B turboshaft, 420 shp (313 kW), derated to 317 shp for takeoff
- Main rotor diameter: 33 ft 4 in (10.16 m)
- Tail rotor diameter: 5 ft 6 in (1.68 m)
Performance
- Maximum speed: 120 kn (138 mph, 222 km/h)
- Cruise speed: 110 kn (127 mph, 204 km/h)
- Range: 374 nmi (430 mi, 690 km)
- Service ceiling: 13,500 ft (4,115 m)
- Rate of climb: 1,350 ft/min (6.9 m/s)
Grumman HU-16 Albatross
The Grumman HU-16 Albatross is a twin-engine amphibious flying boat originally developed in the late 1940s for long-range maritime patrol, search and rescue (SAR), and utility transport missions. It saw extensive service with numerous military operators, including the Royal Canadian Air Force. The Amphibious Training and Laboratory Aircraft System (ATLAS) operated by ITPS (Canada) Ltd. supports the training of seaplane test pilots and is instrumented for flight test data acquisition, including performance, flying qualities, and water handling evaluations. The aircraft also features an external video system for capturing water spray behavior during amphibious operations.
General characteristics
- Crew: two to four (pilot, co-pilot, flight engineer, mission support)
- Capacity: up to 10 passengers or mission equipment
- Length: 62 ft 10 in (19.15 m)
- Wingspan: 96 ft 8 in (29.47 m)
- Height: 25 ft 10 in (7.87 m)
- Empty weight: approx. 24,000 lb (10,886 kg)
- Max takeoff weight: 37,500 lb (17,010 kg)
- Fuel capacity: approx. 880 US gallons (3,330 liters)
- Powerplant: 2 × Wright R-1820-76 Cyclone 9 radial engines, 1,425 hp (1,063 kW) each
- Propellers: 3-bladed constant-speed, fully feathering
Performance
- Maximum speed: 205 kn (236 mph, 380 km/h)
- Cruise speed: 108 kn (124 mph, 200 km/h)
- Range: 2,478 nmi (2,850 mi, 4,590 km)
- Service ceiling: 21,500 ft (6,553 m)
- Rate of climb: approx. 1,000 ft/min (5.1 m/s)
Cirrus SR22
The Cirrus SR22 is a single-engine, four-to-five-seat composite aircraft developed by Cirrus Aircraft. One of the most popular high-performance general aviation aircraft in the world, it features advanced avionics, a glass cockpit, and the Cirrus Airframe Parachute System (CAPS). The SR22 is widely used in pilot training, personal transport, and systems evaluation environments.
General characteristics
- Crew: one
- Capacity: 3–4 passengers
- Length: 26 ft 0 in (7.92 m)
- Wingspan: 38 ft 4 in (11.68 m)
- Height: 8 ft 11 in (2.72 m)
- Empty weight: 2,345 lb (1,064 kg)
- Max takeoff weight: 3,600 lb (1,633 kg)
- Fuel capacity: 92 US gallons (348 liters) usable
- Powerplant: 1 × Continental IO-550-N, 310 hp (231 kW)
- Propeller: 3-bladed constant-speed propeller
Performance
- Maximum speed: 211 kn (243 mph, 391 km/h)
- Cruise speed: 183 kn (211 mph, 339 km/h)
- Range: 1,100 nmi (1,265 mi, 2,040 km) at economy cruise
- Service ceiling: 17,500 ft (5,334 m)
- Rate of climb: 1,270 ft/min (6.5 m/s)
- Takeoff distance: 1,517 ft (462 m)
- Landing distance: 1,178 ft (359 m)
Cessna 414
The Cessna 414 is a pressurized, twin-engine light aircraft developed by Cessna Aircraft Company. Designed for comfortable high-altitude personal and business travel, the 414 offers strong performance and range in a compact package. It is often used in advanced flight training, systems evaluation, and flight test engineering programs due to its complexity, pressurization system, and twin-engine configuration.
General characteristics
- Crew: one or two
- Capacity: up to 6 passengers (typical cabin configuration)
- Length: 36 ft 5 in (11.10 m)
- Wingspan: 44 ft 3 in (13.49 m)
- Height: 11 ft 4 in (3.45 m)
- Empty weight: approx. 4,496 lb (2,039 kg)
- Max takeoff weight: 6,750 lb (3,062 kg)
- Fuel capacity: 206 US gallons (780 liters) usable
- Powerplant: 2 × Continental TSIO-520-J turbocharged flat-six engines, 310 hp (231 kW) each
Performance
- Maximum speed: 235 kn (270 mph, 435 km/h)
- Cruise speed: 220 kn (253 mph, 407 km/h)
- Range: 1,528 nmi (1,759 mi, 2,830 km)
- Service ceiling: 30,800 ft (9,390 m)
- Rate of climb: 1,700 ft/min (8.6 m/s)
- Takeoff distance: ~2,000 ft (610 m) over 50 ft obstacle
- Landing distance: ~2,200 ft (670 m) over 50 ft obstacle
IAR-823 Brasov
The IAR-823 is a Romanian-built, single-engine, low-wing trainer aircraft developed by IAR Brașov. Designed for primary training, aerobatics, navigation, and instrument flying, it was used extensively by the Romanian Air Force and exported to several countries. Its rugged construction, forgiving handling, and side-by-side cockpit make it well-suited for both military and civil flight training applications.
General characteristics
- Crew: two (student and instructor, side-by-side)
- Capacity: up to 2 additional rear passengers in utility/training configuration
- Length: 28 ft 2 in (8.58 m)
- Wingspan: 35 ft 9 in (10.90 m)
- Height: 9 ft 6 in (2.90 m)
- Empty weight: 2,381 lb (1,080 kg)
- Max takeoff weight: 3,858 lb (1,750 kg)
- Fuel capacity: approx. 82 US gallons (310 liters)
- Powerplant: 1 × Lycoming IO-540-G1D5, 290 hp (216 kW)
- Propeller: 3-bladed constant-speed propeller
Performance
- Maximum speed: 192 kn (221 mph, 356 km/h)
- Cruise speed: 170 kn (196 mph, 315 km/h)
- Range: 695 nmi (800 mi, 1,287 km)
- Service ceiling: 20,000 ft (6,100 m)
- Rate of climb: 1,100 ft/min (5.6 m/s)
- Takeoff distance: approx. 1,200 ft (366 m)
- Landing distance: approx. 1,350 ft (411 m)
Manned Remotely Piloted Aircraft (MRPA)
The Manned Remotely Piloted Aircraft (MRPA) Long EZ is a modified canard-configuration experimental aircraft designed to simulate Medium Altitude Long Endurance (MALE) Remotely Piloted Aircraft. It is used to train flight test professionals in the operation and testing of Uncrewed Aerial Systems (UAS) with full human-in-the-loop control via a ground station. The MRPA Long EZ is equipped with a modern Electro-Optic sensor payload and is fully instrumented for flight testing. It can be flown conventionally or remotely from a Ground Control Station (GCS), offering a unique surrogate environment for RPA operations and testing.
General characteristics
- Crew: 1 pilot onboard and remotely operated from GCS
- Configuration: Canard pusher with tandem cockpit
- Length: 17 ft 5 in (5.31 m)
- Wingspan: 26 ft 1 in (7.95 m)
- Height: 6 ft 0 in (1.83 m)
- Empty weight: approx. 710 lb (322 kg)
- Max takeoff weight: approx. 1,325 lb (601 kg)
- Fuel capacity: approx. 52 US gallons (197 liters)
- Powerplant: 1 × pusher engine (Lycoming O-235 or equivalent), approx. 115 hp (86 kW)
Performance
- Maximum speed: 185 mph (160 kn, 298 km/h)
- Cruise speed: 150 mph (130 kn, 241 km/h)
- Range: ~800 nmi (1,480 km)
- Service ceiling: ~25,000 ft (7,620 m)
- Endurance: Up to 6 hours
- Takeoff distance: ~1,000 ft (305 m)
- Landing distance: ~1,200 ft (366 m)
Avionics & Systems (MRPA Configuration)
- Dual-mode control: manned cockpit or GCS-based operation
- Representative Ground Control Station with pilot and payload operator consoles
- Fly-by-wire interface (remote control integration)
- Electro-Optic/Infrared (EO/IR) sensor payload
- Downlink video and telemetry for real-time monitoring
- GPS/INS navigation
- Full flight test instrumentation and data recording system
- Safety monitoring and data link termination capabilities
- RF datalink with command & control redundancy
UAV Fleet
From the outset, students learn that UAS are available in many forms, sizes and of varying complexity. The overall footprint of the system will ultimately determine where the system can be operated from. A Ground Control Station (GCS) may be as simple as a hand-held device or as complex as a full integration into a fixed complex.
Matrice 300 RTK
A professional-grade quadcopter by DJI, the Matrice 300 RTK features advanced AI capabilities, a 55-minute maximum flight time, and a 15 km transmission range. It supports multiple payloads and is ideal for complex sensor evaluations and system performance testing.
Sky Whale Mini
A compact, fixed-wing UAV designed for endurance and portability. With a wingspan of approximately 2 meters and up to 2-hour flight time, it's well-suited for long-range data link evaluation and low-speed handling assessments.
PteroDynamics P4 Transwing
This VTOL aircraft features a unique folding-wing design that enables both vertical takeoff and efficient fixed-wing flight. With speeds up to 100 km/h and 2+ hour endurance, it is used for testing transition flight modes and evaluating aerodynamic behavior in hybrid configurations.
Freespace Operations Callisto 50 MR
A large, heavy-lift multirotor platform designed for versatile payload integration. Capable of lifting over 20 kg and flying for 30–40 minutes, it provides a robust platform for sensor and heavy systems testing.
Mavic 2 Enterprise Dual (Mavic 2ED)
This compact, commercial UAV features integrated visual and thermal imaging cameras. With a 31-minute flight time and 8 km range, it supports real-time visual and infrared inspections, often used for practical EO/IR sensor flight testing.
Mavic Mini 2
A lightweight, sub-250g recreational-class UAV with 31-minute endurance and 10 km transmission range. Though compact, it's used for basic training, initial datalink assessments, and procedural flight tasks due to its ease of deployment and minimal regulatory footprint.
Bombardier Challenger
The Bombardier Canadair Challenger 601 is a Canadian business jet able to accommodate 11 occupants. The aircraft first flew in 1978 and was certified in 1980. The aircraft employed by ITPS C-GORD provides an excellent test pilot training tool with a ceiling of 41000 feet and EFIS equipped cockpit including Flight Management System (FMS) autopilot and weather RADAR. The Challenger 601 has a maximum takeoff weight of 48200 lb. It is powered by two General Electric CF34-3B turbofans, of 9220 lbf thrust each. The aircraft’s performance Maximum speed of 490 KIAS, Mmo of M 0.85 a service ceiling of 41000 feet and range of 4000 nm with reserves.
This aircraft is owned and operated by FlightPath Charter a charter company based in the Region of Waterloo and is operated by ITPS under a commercial agreement with the company.
Embraer Phenom 100
The Embraer Phenom is a Brazilian very light jet (VLJ). It is a modern aircraft certified in 2007 and equipped with the Embraer Prodigy Touch Flight Deck. The aircraft employed by ITPS C-FLOX is well suited for civil test pilot training featuring modern avionics and autopilot and a useful performance envelope. The aircraft is regularly used for performance, flying qualities and avionics systems testing exercises. The EMB 500 has a Maximum Take Off Weight of 10,582 lb. It is powered by two Pratt & Whitney Canada PW617F1-E turbofans. The aircraft’s performance includes a 405 KIAS cruise speed and an Mmo of M 0.7 a service ceiling of 41000 ft and range of 1,178 with reserves.
This aircraft is owned and operated by FlightPath Charter a charter company based in the Region of Waterloo and is operated by ITPS under a commercial agreement with the company.
Embraer Phenom 300
The Embraer EMB-505 Phenom 300 is a Brazilian light jet able to accommodate 11 occupants. The aircraft first flew in 2008 and was certified in 2009. The aircraft employed by ITPS C-FWTF provides an excellent test pilot training tool with a ceiling of 45000 feet and a modern airliner-like glass cockpit and systems, but with much lower operating costs resulting in outstanding training value. The EMB-505 has a maximum takeoff weight of 17,968 lb. It is powered by two Pratt & Whitney Canada PW535E turbofans, of 3,360 lbf thrust each. The aircraft’s performance Maximum speed of 450 KIAS, Mmo of M 0.79 a service ceiling of 45000 feet and range of 1971 nm with reserves. Belgian AF student pictured during his final project evaluation of the Phenom 300.
This aircraft is owned and operated by FlightPath Charter a charter company based in the Region of Waterloo and is operated by ITPS under a commercial agreement with the company.
Diamond DA42-L360
The Diamond DA42 is an all composite, four seat twin engine propeller aircraft. The aircraft features an innovative design and a Garmin G1000 glass cockpit with autopilot. The North American L-360 version is powered by Lycoming gasoline powered engine unlike the European version which is equipped with diesel engines. The aircraft is used at ITPS for Vmca determination demonstrations as well as for performance and flying qualities flight test techniques demonstrations and flight exercises. The glass cockpit also renders it useful for avionics systems and autopilot testing exercises. The DA-42 L360 has a Gross Weight of 3,748 lb and is powered by two Lycoming IO-360 of 180 hp each. The airplane performance includes a maximum speed of 192 KIAS, range of 914 nm and a service ceiling of 18000 ft.
Diamond DA20 C-1 Eclipse
The Diamond Aircraft DA-20 is a two seat all composite general aviation aircraft first flew in 1993. The aircraft features excellent visibility through an aft hinged bubble canopy It is equipped with conventional controls and an analogue cockpit. The DA20 at ITPS is used for flight test techniques demonstrations for flight test engineers and spin testing demonstrations to pilots and engineers. On board data acquisition allows recording of key parameters and reconstruction of the spin post-flight. The DA20 has a Gross weight of 1,764 lb and is powered by a Continental IO-240-B3B four cylinder horizontally opposed piston aircraft engine of 125 hp. The performance includes a cruise speed of 138 KIAS, range of 547 nm and a service ceiling of 13120 ft.
Leonardo AW119Ke Koala
An eight-seat utility helicopter powered by a single turbo-shaft engine for the civil market. Used for Performance, Flying Qualities, test techniques instruction, evaluations/data flights, PORTABLE FLIGHT DATA RECORDER (PFDR), 128 parameters, in flight monitoring of selected parameters.
Airbus Helicopters AS355 TwinStar
The Airbus Helicopters AS355 TwinStar is a light twin-engine utility helicopter developed from the single-engine AS350. It features a high-mounted main rotor, twin turboshaft engines, and a spacious cabin, making it well-suited for IFR training, surveillance, and multi-role utility missions. Its twin-engine redundancy and light handling characteristics also make it a valuable platform for flight test and systems evaluation training.
General characteristics
- Crew: one or two
- Capacity: up to 5 passengers
- Length: 42 ft 5 in (12.93 m) including rotors
- Fuselage length: 35 ft 1 in (10.70 m)
- Height: 10 ft 11 in (3.33 m)
- Empty weight: approx. 2,900 lb (1,315 kg)
- Max takeoff weight: 5,225 lb (2,370 kg)
- Fuel capacity: approx. 160 US gallons (606 liters)
- Powerplant: 2 × Turbomeca Arrius 1A or 1A1 turboshaft engines, 530 shp (395 kW) each (derated)
- Main rotor diameter: 35 ft 1 in (10.69 m)
Performance
- Maximum speed: 155 kn (178 mph, 287 km/h)
- Cruise speed: 130 kn (150 mph, 241 km/h)
- Range: 360 nmi (414 mi, 667 km)
- Service ceiling: 16,000 ft (4,875 m)
- Rate of climb: approx. 1,300 ft/min (6.6 m/s)
- Endurance: approx. 3 hours
Boeing 787 Simulator
B787 Simulator
- 3 Channel 4k 120 hertz display
- Fully representative of modern fly-by-wire transport aircraft
- Fully kitted for engineering training
F-18 Combat Simulator
- 6 channel 4k 120 hertz display (configurable with dome and mixed reality settings)
- Fully functional avionics and weapon system
- Networked to Telemetry room for flight test exercises/rehearsal
F-35 Engineering Simulator
- Real time varying of aerodynamic derivatives
- Functional avionics and panoramic HMD
- Multi-configurable setups including 180-degree screen, and mixed reality
F-16C Combat Simulator
F-16C Viper
- F-16C Simulators based on the Block 50 model
with fully functional and accurate Human
Machine Interface (HMI) - Mixed Reality configurability
- Fully advanced avionics and weapons systems
eVTOL Simulator
The eVTOL engineering simulator was developed to support ITPS UAS/UAM flight testing courses. Connected to our Telemetry Room and Ground Control Station (GCS) with real-time data monitoring by engineers, it allows the rehearsal of piloted, remotely piloted, and autonomous eVTOL flight test operations. The eVTOL simulator cockpit allows for multiple control configurations to evaluate different Human Machine Interface (HMI) strategies. Piloted evaluations feature a mixed reality solution providing a high degree of realism. The design is based on a Bell 206 to represent a machine with potential UAM or utility applications.
AH-64 Apache Simulator
Leonardo AW139 Simulator
The AW139 is a high fidelity customisable rotary wing simulator based on the Entrol H39-EASA FNPT II MCC/ FAA FTD Level 5 simulator. The AW139 simulator is an upgradeable, robust solution with commercial off-the-shelf elements for cost-effective and flexible training.
- Cylindrical dome display with full HD projectors
- Glass cockpit based on Primus Epic system
- Enclosed instructor station with touch screen interface for weather radar and EGPWS
- Control of variable factors such as terrain scenarios, weather, failures and positioning
- Terrain scenarios mission training
