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XC – 30 Dart:
Strategic Airlift Military Transport Vehicle
5/29/2015 1Upward Aviation - Han
XC – 30 Dart Specifications
5/29/2015 2
Engine Type PW2043
Thrust 170,400 lb
Max Payload 300,000 lb
MTOW 732,482 lb
Cruise Mach 0.7
Upward Aviation - Han
Airflow into the Engine at
13° Angle of Attack
5/29/2015 3Upward Aviation - Han
5/29/2015
Cargo Integration
4Upward Aviation - Han
5/29/2015
Cargo Integration
5
Optional Cargo Units
M1AAbrams 1
M2 Bradley 8
M3 Bradley 8
Apache
Helicopter
2
44 Master Pallets
34 463L Master Pallets and
1 M104 Assault Bridges
Upward Aviation - Han
XC-30 Ramp Design
5/29/2015 6
Front Opening
Rear Opening
Side view of with Opening
Utilizing the wide fuselage,
two wide ramps, one in the
front and one in the back, are
used to decrease loading time.
Upward Aviation - Han
Wing Structure
5/29/2015 Upward Aviation - Han 7
• 2 spars, foreword &
aft
─ Al 7055-T6
• False spar for control
surfaces
• 32 stringers, 8”
spacing
─ Carbon Fiber
Reinforced Polymer
─ Integrated with the
wing skin; no need for
fasteners
• 100 ribs, 24” spacing
─ Al 7055-T6
Fuselage Structure
5/29/2015 Upward Aviation - Han 8
• Frames
─Aluminum 7055-T6
─20 inch spacing
• Stringers
─Carbon Fiber Reinforced Polymer (bonded to skin)
─8 inch spacing

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Sample of Work

  • 1. XC – 30 Dart: Strategic Airlift Military Transport Vehicle 5/29/2015 1Upward Aviation - Han
  • 2. XC – 30 Dart Specifications 5/29/2015 2 Engine Type PW2043 Thrust 170,400 lb Max Payload 300,000 lb MTOW 732,482 lb Cruise Mach 0.7 Upward Aviation - Han
  • 3. Airflow into the Engine at 13° Angle of Attack 5/29/2015 3Upward Aviation - Han
  • 5. 5/29/2015 Cargo Integration 5 Optional Cargo Units M1AAbrams 1 M2 Bradley 8 M3 Bradley 8 Apache Helicopter 2 44 Master Pallets 34 463L Master Pallets and 1 M104 Assault Bridges Upward Aviation - Han
  • 6. XC-30 Ramp Design 5/29/2015 6 Front Opening Rear Opening Side view of with Opening Utilizing the wide fuselage, two wide ramps, one in the front and one in the back, are used to decrease loading time. Upward Aviation - Han
  • 7. Wing Structure 5/29/2015 Upward Aviation - Han 7 • 2 spars, foreword & aft ─ Al 7055-T6 • False spar for control surfaces • 32 stringers, 8” spacing ─ Carbon Fiber Reinforced Polymer ─ Integrated with the wing skin; no need for fasteners • 100 ribs, 24” spacing ─ Al 7055-T6
  • 8. Fuselage Structure 5/29/2015 Upward Aviation - Han 8 • Frames ─Aluminum 7055-T6 ─20 inch spacing • Stringers ─Carbon Fiber Reinforced Polymer (bonded to skin) ─8 inch spacing