SM-47 SUPER MACHETE PERFORMANCE & SPECIFICATIONS

LEADING PARTICULARS

MODEL SPECIFIED

SM-47S & SM-47T SUPER MACHETE™

TYPE

SM-47S
SM-47T

Single Seat Light Strike Fighter (LSF)
Two Seat Tandem Light Strike Fighter/Supersonic Trainer

POWERPLANT

Number and Type
Model
Maximum Afterburning Thrust (lbs-sl)
Maximum Military Thrust (lbs-sl)

Single Afterburning Turbofan
GEAE F414-GE-400 Afterburning Turbofan
22,000 lbs
14,756 lbs

ACCOMMODATION

SM-47S
SM-47T

Single Pilot on Martin Baker MK.16E
Two Seat Tandem on Martin Baker MK.16E

RADAR

Multi-Mode Radar

Lockheed Martin AN/APG-67(V4) Multi-Mode

TARGETING SYSTEMS

Targeting Pod/FLIR Option # 1
Targeting Pod/FLIR Option # 2

Rafael LITENING III FLIR (External Hardpoint)
SNIPER Advanced Targeting Pod (External Hardpoint)

HELMET MOUNTED DISPLAY (HMD)

Forward Station Option # 1
Aft Station Option # 1

HEAD UP DISPLAY (HUD)

Forward Station Option # 1
Aft Station Option # 1

VSI F/A-35 HMDS
CMC Electronics Night Hawk Repeater

CMC Electronics Night Hawk
CMC Electronics Night Hawk Repeater

MULTI-FUNCTIONAL DISPLAYS (MFDs)

Multi-Functional Displays

(5) x L3 Actiview 104P 6 x 8 in LCDs

MISSION COMPUTERS

Option # 1
Option # 2
Option # 3

CMC Electronics FV4000 MMDP
GD AN/AYQ-25(V) Advanced Mission Computer
Elbit MDP/MMRC Multi-Role Computer

STORES MANAGEMENT

SMS/WDNS Option # 1
SMS/WDNS Option # 2

GD AIS Stores Management System
Elbit SMS-86 Stores Management System

NAVIGATION SYSTEMS

GPS/INS Option # 1
GPS/INS Option # 2
GPS/INS Option # 3
GPS/INS Option # 4

TACAN Option # 1
TACAN Option # 2

ADF Option # 1
ADF Option # 2

VOR/ILS Option # 1

Radar Altimeter Option # 1

Northrop Grumman LN-260 INS
Raytheon DAR GPS Digital Anti-Jam Receiver
Northrop Grumman AN/ASN-166 GPS/INS
Honeywell H-764G Embedded GPS/INS

AN/ARN-153(V) DME/TACAN
AN/ARN-154(V) TACAN

Collins ADF-462/4000
Honeywell KR 87

Honeywell AN/ARN-147V

Honeywell APN-194

COMMUNICATION SYSTEMS

UHF/VHF COMM Option # 1
UHF/VHF COMM Option # 2
UHF/VHF COMM Option # 3

IFF Transponder Option # 1
IFF Transponder Option # 2
IFF Transponder Option # 3
IFF Transponder Option # 4

Secure Voice Option # 1

Datalink Option # 1

Intercom Option # 1

Emergency Power Option # 1

Cockpit VADR Option # 1

Rockwell Collins AN/ARC-210(V)
Raytheon AN/ARC-232(V) Starblazer
IAI ELTA ARC-740

BAE Systems AN/APX-113(V) CIT
BAE Systems AN/APX-121(V) IFF
Raytheon AN/APX-100(V)
BAE Systems AN/APX-118(V)

Secure Replacement to Raytheon KY-58 SVS

AN/URC-138 Link 16 Low Volume Terminal

Andrea Electronics A301-412 Intercom

PS-855/B Emergency Power Supply

FA2100 Cockpit Voice/Data Recorder

ELECTRONIC WARFARE SUITE

Self-Protection Suite

RF ECM Option # 1

MAWS Option # 1

RWR Option # 1
RWR Option # 2

SPJ Option # 1

LWR Option # 1

Chaff/Flare Dispenser Option # 1

ASPIS

AN/ALQ-187 Internal Countermeasures

Raytheon AN/AAR-58 Advanced MAWS

AN/ALR-93V Radar Warning Receiver
Elisra SPS-65(V) RWR/RWS/SPS

AN/ALQ-165 ASPJ

Elisra LWS-20V-2 Laser Warning System

BAE Systems AN/ALE-47; 10-12 Dispensers

FIXED INTERNAL ARMAMENT

SM-47S
SM-47T

(1) x GD M61A2 20 mm Cannon with 1,000 rds
(1) x GD M61A2 20 mm Cannon with 500 rds

EXTERNAL ARMAMENT

Eight (8) Wing Mounted External Hardpoints for 11,000 lbs Stores/Ordinance Using NATO Standard Lug Suspension

DIMENSIONS

OVERALL (All Models)

Overall Span
Overall Length
Overall Height
Gross Wing Area

36 ft 0 in
40 ft 0 in
12 ft 9 in
309.8 sq ft

WING (All Models)

Leading Edge Sweep
Span
Area
Aspect Ratio
Mean Airfoil

-30°
36 ft 0 in
278.3 sq ft
4.66
6% Supersonic Root/4% Supersonic Tip

CANARD (All Models)

Leading Edge Sweep
Span (unit)
Area
Aspect Ratio
Mean Airfoil

50°
4 ft 6 in
31.5 sq ft
2.57
4% Supersonic Airfoil

HORIZONTAL STABILIZER (All Models)

Leading Edge Sweep
Span (unit)
Area
Aspect Ratio
Mean Airfoil

30°
9 ft 7 in
86.1 sq ft
1.59
4.5% Symmetrical Airfoil

VERTICAL STABILIZER (All Models)

Leading Edge Sweep
Span (unit)
Area
Aspect Ratio
Mean Airfoil

40°
6 ft 6 in
58.3 sq ft
2.88
4.5% Symmetrical Airfoil

LANDING GEAR (All Models)

Wheel Base
Wheel Track
Nose/Main Weight Distribution
Nose Tires
Main Tires
Nose Tire Pressure
Main Tire Pressure

16 ft 0in
10 ft 9 in
21%-79%
(1) x 19.5 x 6.75-8
(2) x 24 x 8.0-13
110 psi
285 psi

CABIN INTERIOR (All Models)

SM-47S (Single Seat)
Cabin length:
Cabin Height-Maximum:
Cabin Width-Maximum:

SM-47T (Two Seat Tandem)
Cabin length:
Cabin Height-Maximum:
Cabin Width-Maximum:

67 in
61 in
32 in

124 in
62 in
32 in

WEIGHTS

SM-47S (Single Seat)

DRY EMPTY WEIGHT

Crewmember & Survival Equipment:
Internal Ammunition:
Unusable Fuel:
Oil & Oxygen:

AIRCRAFT OPERATING WEIGHT

Maximum Internal Fuel (JP-8):

CLEAN TAKE-OFF WEIGHT (CTOW)

Maximum External Load (Warload):

MAXIMUM TAKE-OFF WEIGHT (MTOW)

Maximum Landing Weight (MLW)

Design Load Factor @ MTOW

Ultimate Load Factor @ MTOW

14,478 lbs

260 lbs
557 lbs
40 lbs
10 lbs

15,366 lbs

7,250 lbs

22,616 lbs

11,000 lbs

33,616 lbs

33,616 lbs

7.5

11.5

SM-47T (Two Seat Tandem)

DRY EMPTY WEIGHT

Crewmember & Survival Equipment:
Internal Ammunition:
Unusable Fuel:
Oil & Oxygen:

AIRCRAFT OPERATING WEIGHT

Maximum Internal Fuel (JP-8):

CLEAN TAKE-OFF WEIGHT (CTOW)

Maximum External Load (Warload):

MAXIMUM TAKE-OFF WEIGHT (MTOW)

Maximum Landing Weight (MLW)

Design Load Factor @ MTOW

Ultimate Load Factor @ MTOW

14,749 lbs

520 lbs
577 lbs
40 lbs
20 lbs

15,906 lbs

7,250 lbs

23,156 lbs

11,000 lbs

34,156 lbs

34,156 lbs

7.5

11.5

PERFORMANCE & HANDLING

Performance estimates are based upon a standard SM-47S/T aircraft at CTOW or MTOW as specified. MTOW configuration is representative of an external warload including 6 x AIM-120 and 2 x AIM-9X under ISA, standard day conditions. Takeoff and landing field lengths are based on level, hard surface runways with zero wind. Ferry range is with 4 x 150 USG tanks and 2 x AIM-120.

SM-47S & SM-47T

Max Level Speed @ SL
Max Level Speed @ FL 150
Max Level Speed @ FL 250
Max Level Speed @ FL 350
Supercruise @ FL 250
Supercruise @ FL 350
Cruise Speed @ FL 150
Cruise Speed @ FL 250
Cruise Speed @ FL 350

Stall Speed Flapped @ SL-CTOW
Approach Speed Flapped @ SL-CTOW
Stall Speed Flapped @ SL-MTOW
Approach Speed Flapped @ SL-MTOW

Max Climb Rate @ SL-CTOW
Max Climb Rate @ SL-MTOW

Service Ceiling Exceeds

Tactical Radius; 20 min at Target-MTOW
Cruise Range, Internal Fuel
Cruise Range with 2 x 150 USG External Tanks
Cruise Range with 2 x 330 USG External Tanks

Takeoff Distance-SL-CTOW
Landing Distance-SL-CTOW
Takeoff Distance-SL-MTOW
Landing Distance-SL-MTOW

Wing Loadings (lbs/sq ft)
Thrust-To-Weight Ratios
Design Load Factor-CTOW
Design Load Factor-MTOW

1.21 Mach
1.47 Mach
1.81 Mach
1.83 Mach
1.40 Mach
1.40 Mach
0.85 Mach
0.85 Mach
0.85 Mach

127 Ktas
130 Ktas
138 Ktas
156 Ktas

33,300 ft/min
22,142 ft/min

60,000 ft

760 nm
1,520 nm
2,200 nm
2,700 nm

1,320 ft
1,777 ft
3,041 ft
2,641 ft

70 to 110
1.01 to 0.64
+11.0/-5.5
+7.5/-3.75