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SM-36 Stalma
Aircraft

SM-36 · Stalma Family

Stalma

Reimagined as a sixth-generation MRF. Variable geometry. Mach 2.6+.

Speed

Mach 2.6+

Range

2,324 nm

Warload

20,000 lb

Thrust

52,500 lb

MTOW

65,000 lb

Engine

E1400 VCE

Overview

The SM-36 Stalma is a single engine, afterburning turbofan powered, low-observable Air Superiority and Multi Role Fighter. Variable geometry swing wings, canard foreplanes, internal weapons carriage and thrust vectoring nozzles.

The Multi-Role Fighter is the back-bone of modern air defense. Proficiently satisfying air-to-air and air-to-surface engagements with unprecedented flexibility, the Multi-Role Fighter (MRF) is the leading combat asset of western air forces. The MRF has become the most procured of all fighter types, with over 7,000 MRFs now in service worldwide. Performing critical missions with stunning success, MRFs including the F-4 Phantom II, F-16 Fighting Falcon, and the F/A-18 Hornet and Super Hornet are legendary. The SM-36 Stalma will continue the legend.

Reimagined as a sixth generation MRF developed to succeed both F-16s and F/A-18s while exceeding CTOL F/A-35A/B JSF performance in all regimes, the SM-36 Stalma will be an alluring super-fighter for the 21st century. A synergistic integration of aerodynamics, distinct configuration and the most advanced software driven avionics, sensors and electronic warfare systems, the SM-36 will be a lethal instrument like no other.

The SM-36 is a single engine, single seat (SM-36S) or two seat tandem (SM-36T) MRF. An all-weather platform, primary mission capabilities include Air Superiority (AS), Combat Air Patrol (CAP); Deep Penetration Precision Strike (DPPS) utilizing conventional or nuclear devices; and Close Air Support (CAS). The SM-36 design results in a high performance aircraft with great acceleration, climb and instantaneous turn rates with exceptional maneuverability to fulfill both close-combat/dogfight and air defense roles. Secondary emphasis has focused upon Low Observable (LO) features and supercruise.

The SM-36 Stalma is a single engine, afterburning turbofan powered, Lo-Observable Air Superiority and Multi-Role Fighter. Equipped with variable geometry swing wings, canard foreplanes, internal weapons carriage and thrust vectoring exhaust nozzles, the SM-36 is a Mach 2.6+, super-maneuverable, supercruise fighter intended to replace F/A-18E/Fs and F/A-35s. Offering a lower RCS, superior avionics and powerplants and greater performance than the F/A-35, the SM-36 is now being reimagined by Stavatti as a sixth generation fighter. Engineered to meet near term next generation fighter needs to fill immediate capability gaps, the prototype and final production configuration of the SM-36 is highly proprietary and restricted for both business defense security purposes. Published SM-36 arrangement drawings and artist renderings may not be indicative of prototype and aircraft final production configuration.

Gallery

Authentic Stavatti imagery.

SM-36 Stalma Hellenic Air Force
SM-36 Stalma Hellenic Air Force
SM-36 Stalma JASDF
SM-36 Stalma JASDF

Variants

One airframe. Multiple missions.

SM-36S

Single Seat

Air superiority, CAP, deep penetration precision strike, and CAS.

SM-36T

Two Seat

Tandem multi-role fighter.

SM-36U

Uncrewed

Autonomous multi-role fighter sharing the piloted airframe.

Data

Specifications and performance.

SM-36 Stalma

Aircraft

Aircraft
SM-36 Stalma multi-role fighter
Manufacturer
Stavatti Aerospace Ltd
Unit flyaway cost
$50,000,000
First flight
Contact Stavatti
Availability
Pre-Order Today to Secure Delivery Slot
Crew
Single pilot, Martin Baker MK18 zero-zero seat

Dimensions

Max wingspan
64 ft 0 in
Length
58 ft 0 in
Height
13 ft 6 in
Wing area
580 sq ft
Wing aspect ratio
7.06
Wing LE sweep
5° minimum / 70° maximum

Powerplant

Number
1
Type
Afterburning turbofan
Model
E1400-NT-520
Manufacturer
NeoThrust
Afterburning / military thrust
52,500 / 42,700 lbs
Inlet / nozzle
External compression / VG thrust vectoring

Weights

Empty
24,000 lbs
Max internal fuel
20,000 lbs
Max external warload
20,000 lbs
Mid-mission weight
37,000 lbs
Max takeoff weight
65,000 lbs

Loadings

Wing loading (MMW / MTOW)
63.8 / 112.1 lbs/sq ft
Thrust to weight (MMW / MTOW)
1.41 / 0.80
Design / ultimate load factor
+8.33 / +12.5

Armament

Fixed internal
1 × 20 mm M61A2
Ammunition
1,000 rds
Stores stations
6
Max warload
20,000 lbs

Performance

Max level speed at SL
1.25 Mach
Max level speed at FL350 / FL500
2.60 / 2.90 Mach
Supercruise at FL350 / FL500
1.20 / 1.80 Mach
Typical cruise
0.85 Mach
Takeoff / stall speed (MTOW)
162 / 147 KTAS
Approach / stall (landing)
116 / 97 KTAS
Max climb at SL
75,000 ft/min
Service ceiling
75,000 ft
Supercruise range / radius
1,577 / 662 nm
0.85 Mach range / radius
2,324 / 976 nm
Ferry range
3,400 nm
Takeoff ground roll / over 50 ft
1,399 / 1,822 ft
Landing ground roll / over 50 ft
1,278 / 1,417 ft

Avionics & Electronic Warfare

Radar
PhantomStrike AESA
IRST
EOTS
HUD
CED, HMD or LiteHUD
Comm
AN/ARC-210 Gen V
IFF
AN/APX-125
Data link
TACR-16DL
GPS/INS
FALCN
TACAN
AN/ARN-153(V)
RF ECM
AN/ALQ-211A(V)4
MAWS
AN/AAR-58
SPJ
AN/ALQ-214(V)4/5
Chaff/flare
AN/ALE-47

Literature

Linecards and datasheets.

All literature