Initializing Parametric Design Lab
Configuration
Wing Type
Quad
Hex
Octo
Delta
Swept
Canard
Flying Wing
Blended
Tandem
Ring Wing
Box Wing
Biplane
Joined Wing
X-Wing
Tilt-Rotor
Symmetry
Bilateral
Radial
Asymmetric
Scale Factor
1.00x
Airframe Dimensions
Wingspan / Diagonal (mm)
297
Fuselage Length (mm)
100
Wing Sweep Angle (deg)
0
Wing Aspect Ratio
4.0
Wing Taper Ratio
1.00
Dihedral (deg)
0
Propulsion
Engine Type
Brushless
Ducted Fan
Micro-Turbojet
Pulse Det.
H2 Fuel Cell
Hybrid E-Jet
Ramjet
Solar-Elec
Wankel
Turboprop
Engine Count
4
Engine Placement
Distributed
Tractor
Pusher
Wingtip
Overwing
Underwing
Centerline
Vectored
Payload
Payload Type
Kinetic
Net Capture
Blast-Frag
Cont. Rod
EW Jammer
Dir. Energy
Marker
Tangle Wire
EFP
None
Payload Mass (g)
48
Seeker Type
None
FPV Cam
IR
Radar
LIDAR
IR+Radar
Visual AI
Acoustic
Materials
Primary Structure
Carbon Fiber
Aluminum
Titanium
3D PLA
3D Nylon
3D PETG
Kevlar
Fiberglass
Foam Core
Balsa
Origami Fold
Inflatable
Surface Treatment
Raw
Painted
RAM Coating
Ceramic
Ablative
Battery / Fuel
Energy Source
LiPo
LiHV
Li-Ion
Solid State
H2 Tank
JP-8
Solar
Supercap
Zinc-Air
Energy Capacity (Wh)
19

Design Summary

ConfigQuad
AUW544 g
T/W7.2
Max Speed180 km/h
Endurance4.5 min
CostEUR 260
Aerodynamics
Wing Area0.053 m2
Wing Loading-- N/m2
Aspect Ratio4.0
CL max0.80
CD00.400
L/D max--
Stall Speed-- km/h
Max Speed-- km/h
Reynolds (cruise)--
Performance
Cruise Speed-- km/h
Rate of Climb-- m/s
Service Ceiling-- m
Endurance-- min
Range-- km
Max G-- G
Turn Radius (max G)-- m
T/W Ratio--
Structural
Empty Mass-- g
MTOW-- g
Safety Factor--
Nat. Freq. (1st)-- Hz
Mission
Intercept @ 1km-- s
Intercept @ 5km-- s
Kill Probability--%
Detect. Index--
Cost Estimate
Airframe--
Propulsion--
Electronics--
Payload--
Total Unit Cost--
Performance Radar

Design Comparison