
Length
70 ft
Span
53 ft
Speed
Mach 4.2
Ceiling
> 100,000 ft
Warload
25,000 lb
Thrust
104,800 lb
Overview
The SM-39 is a next generation air dominance fighter and fighter bomber. Twin engine, piloted or unpiloted autonomous, low observable. A sixth-generation fighter and a direct bridge between atmospheric aircraft and future reusable space fighters.

The SM-39 is a next generation air dominance fighter and fighter-bomber. Designed to perform the missions of the F-47, F-22, F-15, F/A-18E/F and the now retired F-14 Tomcat, A-5 Vigilante and A-6 Intruder, the SM-39 is a twin engine, piloted or unpiloted autonomous, low observable aircraft. With two internal weapon bays, all moving horizontal stabilizers with no vertical tail, double slotted flaps with boundary layer blowing, thrust vectoring nozzles and titanium foam metal sandwich construction, the SM-39 is a sixth generation fighter and a direct bridge between atmospheric aircraft and future reusable space fighters.
Of radical planform, the SM-39 is a triple fuselage design featuring a streamlined center, high fineness ratio primary fuselage accompanied laterally by right and left mounted secondary fuselages. The secondary fuselages begin as highly swept wing strakes into which the aircraft wing, empennage, a single ventral air intake and engine nacelle is blended. This planform configuration results in a significant reduction in supersonic wave-drag, allowing the aircraft to have a volume distribution that is very near the Sears-Haack ideal. Designed for supercruise, this configuration places the wing leading edge within the shock cone of the secondary fuselage wing strakes at high Mach numbers.
In addition to reducing wave drag, the SM-39’s triple fuselage design allows for an efficient distribution of primary aircraft systems. The center fuselage houses principal avionics, including the radome and AESA radar, as well as the cockpit, nose landing gear and two internal weapons bays. The secondary fuselages house the engines, main landing gear and fuel.
Pioneering new approaches in aerodynamics, airframe structures, efficient variable cycle turbine propulsion, active low-observability and boundary layer control and integrated avionics, the SM-39 is a Mach 4.0+ fighter capable of level supercruise speeds in excess of Mach 2.5 while maintaining a stall speed as low as 103 KTAS in the landing configuration. With a typical per unit flyaway cost of $85 Million, the SM-39 will be competitively priced and offer significant cost savings over same class aircraft. The SM-39 is now under development and will be qualified and certified to MIL-HDBK-516B Airworthiness Certification Criteria in accordance with AFPD 62-6 and AFI 62-601 at the AFFTC, Edwards AFB.
The SM-39 Razor is a sixth generation twin engine Air Superiority and Air Dominance Fighter. A Penetrating Counter Air solution and Fighter Bomber, the SM-39 is designed for both land and carrier based operations. Powered by two next generation variable cycle afterburning turbofans, the SM-39 will have a maximum level speed in excess of Mach 4.0, a tactical radius greater than 1,100 nm, internal weapons carriage, directed energy weapons, supercruise and super-maneuverability. The SM-39 will replace F-22 Raptors, F-15s, Su-57s and Su-27s. The SM-39 design is currently being optimized for improved high speed aerodynamics, reduced over-pressure sonic boom and enhanced low observability characteristics including active signature reduction.
Gallery
Authentic Stavatti imagery.












Variants
One airframe. Multiple missions.
SM-39S
Single Seat
Air superiority / air dominance fighter. Baseline Block 10.
SM-39T
Two Seat
Tandem strike and conversion trainer with full combat fit.
SM-39U
Uncrewed
Autonomous air dominance via Synthetic Intelligence architecture.
Data
Specifications and performance.
SM-39 Razor
Aircraft
- Aircraft
- SM-39 Razor air dominance fighter
- Manufacturer
- Stavatti Aerospace Ltd
- Unit flyaway cost
- $85,000,000
- First flight
- Contact Stavatti
- Availability
- Pre-Order Today to Secure Delivery Slot
- Crew
- Single (S) or two seat (T), MK18 or ACES 5
Dimensions
- Wingspan
- 53 ft 0 in
- Length
- 70 ft 0 in
- Height
- 13 ft 8 in
- Wing area
- 1,026 sq ft
- Wing aspect ratio
- 2.74
- Wing LE sweep
- 50.0°
Powerplant
- Number
- 2
- Type
- Afterburning turbofan
- Model
- E1400-NT-520
- Manufacturer
- NeoThrust
- Afterburning / military thrust (each)
- 52,400 / 42,700 lbs
- Inlet / nozzle
- Internal compression / LO VG thrust vectoring
Weights
- Empty
- 44,500 lbs
- Max internal fuel
- 30,000 lbs
- Max external warload
- 25,000 lbs
- Typical combat weight
- 66,000 lbs
- Max takeoff weight
- 100,500 lbs
Loadings
- Wing loading (TCW / MTOW)
- 64.3 / 98.0 lbs/sq ft
- Thrust to weight (TCW / MTOW)
- 1.59 / 1.04
- Design load factor (TCW / MTOW)
- 11.4 g / 7.5 g
Armament
- Fixed internal
- 1 × 20 mm M61A2 or directed energy
- Ammunition
- 1,000 rds
- Stores stations
- 6
- Max warload
- 25,000 lbs
Performance
- Max level speed at SL
- 1.40 Mach
- Max level speed at FL600
- 4.20 Mach
- Supercruise at FL400
- 2.00 Mach
- Takeoff / stall speed (MTOW)
- 152 / 138 KTAS
- Approach / stall (TLW)
- 115 / 96 KTAS
- Max climb at SL
- > 99,485 ft/min
- Service ceiling
- > 100,000 ft
- Max speed range, internal fuel
- 1,277 nm
- Supercruise range / radius
- 1,700 / 750 nm
- 0.85 Mach range / tactical radius
- 2,419 / 1,300 nm
- Air superiority radius
- 1,400 nm
- 0.85 Mach ferry range
- 5,200 nm
- Takeoff / landing ground roll
- 946 / 1,501 ft
Avionics & Electronic Warfare
- Radar
- ARACR AESA
- IRST
- EOTS or AEOTS
- HUD
- CED or HMD
- Comm
- AN/ASQ-242 or ACNI
- IFF
- AN/ASQ-242 or ACN
- Data link
- AN/ASQ-242 or ACN
- GPS/INS
- FALCN
- RF ECM
- AN/ASQ-239 or AFIDEWS
- MAWS
- AN/ASQ-239 or AFIDEWS
- DAS
- AN/ASQ-239 or ADAS
- SPJ
- AN/ASQ-239 or AFIDEWS
- Chaff/flare
- AN/ALE-52