Good Stuff Happens in 1:1 Meetings: Why you need them and how to do them well
Senior Design Expo Poster
1. TITAN Heavy Lift Transport
Team Members: Brian Lozano, Christian Hoover, Daniel Bavaro
Garett Williams, Michael Nelson, Ryan Mueller
Project Manager: William Kelley
Chief Engineer: Charles Russo
Motivation
• To design a heavy lift transport capable of
transporting a maximum payload of 300,000 lbs
• Primarily a C-5 and C-17 Replacement
Design Process
Aircraft Configuration Landing Comparisons
Loading Capabilities
• TITAN was design to minimize takeoff distance
• Maximum takeoff distance is 4549’
• Smaller takeoff distance then the C-5 & C-17
military transport aircraft
Size Comparisons
2 GE-9X
Engines
Modified H
Tail
Forward Swept
Wings
Advanced
Winglets
Payload Range
• Chart provides range for all the design payload
ranges
• Range and combat radius with a mission
payload of 120,000 lbs
Costs
AE-4350 Team 3
Advanced Composite Frame
Component Weights
3 View
Unrefueled Radius
6,200 nmi
Unrefueled Range
12,800 nmi
•14.5 MMH/FH results in lower flying hour cost than C-17
•Life Cycle Cost of $123.3 Billion
•120 Units Requested
Component Weight (lbs) Component Weight (lbs)
Structural Weight Empty Weight 321580.0
Fuselage 110404.0
Horizontal Tail 10295.0 Cockpit Crew 675.0
Vertical Tail 1 3810.5 TFO 1503.0
Vertical Tail 2 3810.5
Wing 108227.0 Operating Weight
Nose Gear 7088.4 Mission Payload 120000.0
Main Gear Bogie 1 14176.8 Maximum Payload 315000.0
Main Gear Bogie 2 14176.8 Mission Payload Fuel 290447.0
Surface Controls 8094.0 Maximum Payload Fuel 101550.6
Total Structural Weight 280083.0 WE + Fuel 423130.6
WE + Fuel+ PL 636580.0
Powerplant Weight WE + Max. PL + Fuel 731567.6
Engine 1 12400.0
Engine 2 12400.0
Total Poweplant Weight 24800.0
Fixed Component Weight
Fuel System 2515.0
Auxiliary Power 768.0
Instruments 1376.0
Furnishings 3357.0
Electric 4801.0
Avionics 3432.0
Anti Ice 444.0
Total Fixed Component Weight 16693.0
Component Value Unit Component Value Unit
Gross Weight 731,000 lbs Crew 2 + 1 ~
Empty Weight 318,000 lbs Passengers 75 ~
Max Payload 315,000 lbs Cruise Mach 0.76 ~
Fuel Load 320,000 lbs Max Range 15,300 Nmi
Height 56 ft Endurace Mach 0.58 ~
Length 266 ft Max Endurance 35 Hours
Width 31'-8" ft Max Altitude 39,000 ft
Wing Area 7316 ft2
Landing Distance 2,985 ft
Wing Span 271.9 ft Takeoff Distances 4,549 ft
Aircraft Data