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SM-39 Razor
Aircraft

SM-39 · Razor Family

Razor

Mach 4 air dominance. No vertical tails. No compromise.

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.

SM-39 Razor isometric drawing
SM-39 Razor isometric drawing

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.

SM-39 Razor U.S. Navy carrier
SM-39 Razor U.S. Navy carrier
SM-39 Razor carrier approach
SM-39 Razor carrier approach
SM-39 Razor RSAF
SM-39 Razor RSAF
SM-39 Razor JASDF NGAD 012
SM-39 Razor JASDF NGAD 012
SM-39 Razor RCAF
SM-39 Razor RCAF
SM-39 Razor Indian Air Force
SM-39 Razor Indian Air Force
SM-39 Razor rendering 116
SM-39 Razor rendering 116
SM-39 Razor USN NGAD 168
SM-39 Razor USN NGAD 168
SM-39 Razor NGAD ROKAF taking off 112
SM-39 Razor NGAD ROKAF taking off 112
SM-39 Razor NGAD JASDF 008
SM-39 Razor NGAD JASDF 008
SM-39 Razor NGAD USAF 005
SM-39 Razor NGAD USAF 005
SM-39 Razor carrier rendering 148
SM-39 Razor carrier rendering 148

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