This document contains technical specifications and measurements for an aircraft. It lists dimensions, weights, component masses and moments, limits for center of gravity, and notes this is for an academic project by team 211 from UC Davis using an O.S. 0.46 engine and 12x6 propeller. Key data points include an empty weight of 10.33 lbs, wing span of 102.58 inches, and static cargo bay volume of 30.93 cubic inches.

1. 26.87
38.75
2.27
8.81
3.03
10.00
4.50
-4°
21.00
3.92 18.25
47.82
102.58
37.00
15.00
10.00
3.54
4.27
5.00
15.00
17.25
15.74
3.25
12.14
20.13
16.14
Empty CG
Fore CG Limit
Aft CG Limit
Max Load CG
A
All dimensions are in
inches unless noted.
Empty Weight 10.33 lbs
Wing Span 102.58 in
Tail Span 37.00 in
Static Cargo Bay
Volume 30.93 in^3
Propeller 12x6
Engine O.S. 0.46
Key Features
Component Mass (lbs)
Moment Arm with
Respect to Datum
A (in)
Moment (lb in)
Wing 4.69 8.39 39.3491
Fuselage .81 15.5 12.555
Empennage 1.20 47.82 57.384
Engine 1.23 0.875 1.07625
Battery 0.47 9.25 4.3475
DAS 0.47 9.25 4.3475
Empty Fuel Tank 0.08 4.5 0.36
Rear Gear 1.32 18.25 24.09
Front Gear 0.06 3.92 0.2352
Total 10.33 Total Moment
about CG (lb in) 143.74455
Empty CG (in) Fore CG Limit (in) Aft CG Limit (in) Max Loaded CG
(in)
15.74 12.14 20.13 16.14
4
A
123
B B
A
2 134
UC Davis Team # 211
Advanced Modeling
Aeronautis Team
1Taranis
SHEET 1 OF 1SCALE: 1:15 WEIGHT:
REVDWG. NO.
B
SIZE
TITLE:
SOLIDWORKS Student Edition.
For Academic Use Only.