 |
|
 |
|
 |
|
 |
|
 |
|
|
 |
|
 |
|
LEADING PARTICULARS
|
MODEL SPECIFIED
|
SM-72 Tactical Transport™
|
|
TYPE
SM-72
|
Tactical Transport & Theater Airlifter
|
|
POWERPLANT
Number and Type
Model
Maximum SHP @ RPM
Propeller
Propeller Diameter
|
Twin Engine Turboprop
Motor Sich/ZMDB Progress D-27 Turboprop
2 x 14,500 SHP @ 1,000 RPM
Hamilton Standard 8-Blade Scimitar
17 ft 6 in
|
|
ACCOMMODATION
Flight Crew
Troops, Military Configuration
Paratroops, Military Configuration
Medical Litters, Military Configuration
Passengers, First Class Configuration
Passengers, Business Class Configuration
Max Number of 88" x 108" 463L Pallets
Max Number of HMMWVs (Humvees)
|
3-5 with Minimum 2 member flight crew
136
96
110
102
152
7
4
|
|
RADAR
Radar Option # 1
|
Northrop Grumman AN/APN-241 Color Weather Radar
|
|
HEAD UP DISPLAY (HUD)
Pilot & Copilot HUD Option # 1
|
Honeywell Visual Guidance System Head-Up Display
|
|
MULTI-FUNCTIONAL DISPLAYS (MFDs)
Primary MFDs Option # 1
|
(6) x Honeywell Primus Epic 10 x 13 in MF LCDs
|
|
MISSION COMPUTERS
Option # 1
Option # 2
Option # 3
|
Sierra Technologies AN/APN-243(V) Station Keeping
Lockheed Martin Mission Computer
GD AN/AYQ-25(V) Advanced Mission Computer
|
|
NAVIGATION SYSTEMS
GPS/INS Option # 1
GPS/INS Option # 2
GPS/INS Option # 3
GPS/INS Option # 4
TACAN Option # 1
ADF Option # 1
ADF Option # 2
VOR/ILS Option # 1
Radar Altimeter Option # 1
|
Raytheon DAR GPS Digital Anti-Jam Receiver
Northrop Grumman LN-100G GPS/INS
Northrop Grumman LN-93 INS
Honeywell H-764G Embedded GPS/INS
Rockwell Collins AN/ARN-153(V) TACAN
Collins ADF-462/4000
Honeywell KR 87
Honeywell AN/ARN-127
Honeywell HG-9550
|
|
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
Secure Voice Option # 1
Datalink Option # 1
Intercom Option # 1
Cockpit VADR Option # 1
|
Rockwell Collins AN/ARC-210(V)
Raytheon AN/ARC-222 VHF/SINCGARS Radio
Raytheon AN/ARC-232(V) Starblazer
Raytheon AN/APX-119
BAE Systems AN/APX-117(V)
BAE Systems AN/APX-118(V)
Secure Replacement to Raytheon KY-58 SVS
MIS/LVT Low-Volume LINK 16
Andrea Electronics AN/AIC-18 Intercom
L3 Aviation Recorders FA2200 MADRAS
|
|
ELECTRONIC WARFARE SUITE
MAWS Option # 1
MAWS Option # 2
RWR Option # 1
RWR Option # 2
IRCM Option # 1
IRCM Option # 2
IRCM Option # 3
Cost Plus SPJ Option # 1
LWR Option # 1
Chaff/Flare Dispenser Option # 1
|
ATK Mission Systems AN/AAR-47 Advanced MAWS
Raytheon AN/AAR-58 Advanced MAWS
BAE Systems AN/ALR-56M RWR
AN/ALR-69 Enhanced RWR
BAE Systems AN/ALQ-157(M) IRCM
Northrop Grumman AN/AAQ-24(V) Nemesis
Northrop Grumman LAIRCM
Northrop Grumman AN/ALQ-165
Elisra LWS-20V-2 Laser Warning System
BAE Systems AN/ALE-47; 10 Dispensers
|
|
|
 |
|
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
|
|
|
DIMENSIONS
|
OVERALL
Overall Span
Overall Length
Overall Height
Gross Wing Area
|
148 ft 0 in
109 ft 0 in
40 ft 9 in
2,470 sq ft
|
|
WING
Leading Edge Sweep
Span
Area
Aspect Ratio
Mean Airfoil
|
-12.5º inboard, 19º outboard
148 ft 0 in
2,470 sq ft
8.87
15% Stavatti Hi-Lift Airfoil
|
|
HORIZONTAL STABILIZER
Leading Edge Sweep
Span
Area
Aspect Ratio
Mean Airfoil
|
-15° inboard, 17.2º outboard
74 ft 6 in
795.6 sq ft
6.98
NACA 0012 Modified
|
|
VERTICAL STABILIZER
Leading Edge Sweep
Span
Area
Aspect Ratio
Mean Airfoil
|
21.4°
24 ft 2 in
344 sq ft
1.68
NACA 0012 Modified
|
|
LANDING GEAR
Wheel Base
Wheel Track
Nose Tires
Main Tires
Nose Tire Pressure
Main Tire Pressure
|
42 ft 1 in
48 ft 6 in
(2) x Type VII 39 x 13, 16 ply
(8) x Type VII 40 x 14, 24 ply
115 psi
170 psi
|
|
INTERIOR CABIN/CARGO HOLD
Cargo Hold Maximum Length:
Cargo Hold Maximum Width:
Cargo Hold Maximum Height:
Cargo Hold Useful Floor Area:
Cargo Hold Volume:
|
58 ft 0 in
15 ft 6 in
11 ft 6 in
623 sq ft
9,500 cu ft
|
|
|
 |
|
 |
|
|
WEIGHTS
Dry Empty Weight
Aircraft Operating Weight
Standard Internal Fuel (JP-8)
Maximum Internal Fuel (Zero Payload; JP-8)
Maximum Payload (With Standard Internal Fuel)
Maximum Take-Off Weight (MTOW)
Maximum Landing Weight (MLW)
|
106,165 lbs
108,105 lbs
52,000 lbs
105,000 lbs
53,000 lbs
213,105 lbs
213,105 lbs
|
|
|
|
 |
|
 |
|
|
PERFORMANCE & HANDLING
Performance estimates are based upon a standard SM-72 aircraft at CTOW or MTOW as specified. MTOW configuration is representative of a Maximum Internal Payload of 53,000 lbs carried within the Aircraft Cargo Hold. under ISA, standard day conditions. Takeoff and landing field lengths are based on level, hard surface runways with zero wind. Ferry range is with Zero Payload and Maximum Fuel (including standard internal fuel plus fuel within CRT offload fuel tanks).
Max Level Speed @ SL
Max Level Speed @ FL 150
Max Level Speed @ FL 250
Economy Cruise Speed @ FL 150
Stall Speed Flapped @ SL-MTOW
Approach Speed Flapped @ SL-MTOW
Stall Speed Clean @ SL-MTOW
Max Climb Rate @ SL-MTOW
Service Ceiling Exceeds
Maximum Endurance, Standard Internal Fuel
Cruise Range, Standard Fuel (52,000 lbs)
Ferry Range, Maximum Fuel (105,000 lbs)
Takeoff Distance-SL-MTOW
Landing Distance-SL-MTOW
Maximum Wing Loading (lbs/sq ft)
Maximum Power Loading (lbs/SHP)
Design Load Factors-MTOW
|
375 KTAS
390 KTAS
380 KTAS
300 KTAS
80 KTAS
95 KTAS
130 KTAS
3,000 ft/min
30,000 ft
12.25 Hours
3,050 nm
6,100 nm
1,350 ft
1,780 ft
86.3
7.4
+4.5/-2.0
|
|
|
 |
 |
|
|
 |
|
|
|
|
|
|
|
|
|
|
|
