Mass Balance - Rocket Glider Project
Content
Initial Component Mass (g) Position (cm) Moment (cm-g) C11-3 32.1 Payload 113.398 Wings Fuselage Nose Cone Stabilizer Total 145.498 0 0 Final Component Mass (g) Position (cm) Moment (cm-g) C11-3 19.7 Payload 113.398 Wings Fuselage Nose Cone Stabilizer Total 133.098 0 0
Design Element Eject Engine Slide Wing Hinged Wing Central Pivot Flex Wing Control Surface Shift Forward Engine Mount Aft Engine Mount Flat Plate Airfoil Dihedral Straight Swept Tapered AR Canard Elevator V tail
Weight
Control
Ease of Construction
Total
Design Element Eject Engine Slide Wing Hinged Wing Central Pivot Flex Wing Control Surface Shift Forward Engine Mount Aft Engine Mount Flat Plate Airfoil Dihedral Straight Swept Tapered AR Canard Elevator V tail
Weight
Control
Ease of Construction
Total
