Mikoyan Gurevich MiG-21UM

Crew 2 The MiG-21UM “Mongol-B” is a tandem two-seat single-engine supersonic jet fighter-trainer operating under an Experimental Airworthiness Certificate. The NTPS MiG-21 is used for Performance, Flying Qualities and Qualitative Evaluation instruction as well as transonic and supersonic student flight test evaluations.
Manufacturer Mikoyan-Gurevich OKB
Country of Origin USSR
Engine Tumansky R-11F2S-300
Thurst (mil) 39.9 kN
Thurst (max) 63.7 kN
Wing Span 7.15 m
Length 4.81 m
Wing Area 23 m2
MTOW 8000 kg
Fuel 2030 kg
Max Load Factor 7 Gs
Vne 1,175 Kias
Climb Rate (Sea Level) 29,530 ft/min
Service Ceiling 17,300 m

 

Aermacchi MB-326M (x3)

Crew 2 The Aermacchi MB-326 “Impala” is a single-engine jet trainer operating under an Experimental Airworthiness Certificate. Some aircraft are instrumented with the ability to perform loads, flutter and spin test flights. The NTPS MB-326s are primarily used for Performance and Flying Qualities flight test instruction
Manufacturer Aermacchi
Country of Origin Italy
Engine Rolls Royce Viper MK22-1
Thurst (mil) 2,500 lbs
Height 12ft 2 in
Wing Span 35 ft 7 in
Length 34 ft 11 in
Wing Area 208.3 ft2
MTOW 9600 lbs
Fuel 368 gal
Range 1,320 nm
Vne 0.82 Mach
Climb Rate (Sea Level) 6,050 fpm
Service Ceiling 47,000 ft

 

Northrop T-38

Crew 2 The Northrop T-38 “Talon” is a tandem two-seat twin-engine supersonic jet trainer operating under an Experimental Airworthiness Certificate. The NTPS T-38 is used for Performance and Flying Qualities instruction as well as transonic and supersonic student flight test evaluations.
Manufacturer Northrop
Country of Origin USA
Engine 2 x General Electric J85-5
Thurst (mil) 2 x 2,050 lbs
Thurst (max) 2 x 2900 lbs
Wing Span 25 ft 3 in
Length 46 ft 4.5 in
Wing Area 170 ft2
MTOW 12,093 lbs
Fuel 583 Gal
Range 991 nm
Vne 746 kts / 1.3 M
Climb Rate (Sea Level) 33,600 ft/min
Service Ceiling 50,000 ft

 

North American NA-265

Crew 2 The North American NA-265 “Sabreliner” is a twin-engine business jet operating under an Experimental Airworthiness Certificate. The NTPS Sabreliner is instrumented and serves as a flying laboratory with flight test engineer consoles. NTPS uses the Sabreliner for Performance and Flying Qualities flight test instruction.
Passenger 6
Manufacturer North American
Country of Origin USA
Engine 2x Pratt &Whitney JT-12A-8
Thurst (mil) 3,300 lbs
Length 44 ft
Height 16 ft
Wing Span 44 ft 6 in
Wing Area 342.1 ft2
MTOW 20,172 lbs
Range 2,170 nm
Vne 478 kts
Service Ceiling 17,300 m

 

Cirrus SR-22 (x3)

Crew 1 The Cirrus SR-22 is a single-engine low-wing composite aircraft operating under an Experimental Airworthiness Certificate. The SR-22s are Technologically Advanced Aircraft (TAA) with modern avionics, GPS and glass panel displays. NTPS operates the SR-22s throughout Systems, Performance and Flying Qualities flight test instruction.
Passenger 2
Manufacturer Cirrus
Country of Origin USA
Engine Continental IO-550-K
Power 315 hp
Length 26 ft
Fuel 92 gal
MTOW 3,400 lbs
Range 1,049 NM
Criuse Speed 183 kts
Climb Rate (Sea Level) 1,270 ft/m
Service Ceiling 17,500 ft