Modular Part Catalog

Build with 1000+ precision parts

Design complex aircraft using our extensive library. From turbine engines to avionics bays, every component is built for realistic flight physics and modular integration.

MODULE 01 / AERODYNAMICSCFD SIMULATED

Variable-Geometry Wing Systems

Optimize your lift-to-drag ratio with procedural wing geometry. Adjust sweep, camber, and span in real-time to test performance across subsonic and supersonic flight envelopes.

  • Procedural wing shaping for custom lift curves
  • Integrated control surfaces for high-G maneuvers
  • Real-time airflow visualization for drag analysis
Wing Profiles:
Aero Telemetry // Lift Data
CFD ACTIVE
Lift Coeff2.4CL VALUE
Drag Index0.1CD VALUE
Stall Angle22DEGREES
Structural Integrity100% Load
Physics Engine: AeroCore v4
0.1ms Calc
MODULE 02 / PROPULSIONTURBINE TECH

High-Bypass Turbofan Engines

Select from a range of turbine engines. Customize intake diameter, bypass ratio, and exhaust nozzle geometry to balance thrust output against fuel consumption.

  • Modular engine mounting for multi-engine setups
  • Variable thrust vectoring for advanced flight
  • Detailed fuel flow and thermal telemetry
Engine Matrix // Turbofan
MAX THRUST
W / SPitch Control
Analog
A / DRoll Control
Analog
Q / EYaw Control
Analog
SpaceThrust Toggle
Binary
GLanding Gear
Toggle
FFlap Adjust
Step
THRUST: 45kNTEMP: 850CFUEL: 12kg/s
MODULE 03 / AVIONICSDIGITAL BUS

Integrated Avionics & Flight Computers

Equip your aircraft with advanced flight computers. Manage navigation, weapon systems, and sensor arrays through a fully customizable digital bus interface.

  • Customizable HUD layouts for flight data
  • Automated flight path stabilization
  • Sensor fusion for target acquisition

Precision Navigation

Real-time GPS and inertial navigation systems for accurate waypoint tracking.

Avionics Bus Telemetry
BUS STABLE

Aero-Hub Alpha

Bus Load: 12%

2 msStable

Aero-Hub Beta

Bus Load: 18%

4 msStable

Aero-Hub Gamma

Bus Load: 22%

5 msStable

Aero-Hub Delta

Bus Load: 15%

7 msStable
Latency: 0.02msBus Sync Active
MODULE 04 / LANDING GEARPROCEDURAL

Procedural Landing Gear Systems

Design custom landing gear configurations. From simple tricycle setups to complex multi-wheel bogies, our procedural system adapts to your fuselage design.

  • Adjustable strut length and suspension stiffness
  • Retractable mechanisms with custom timing
  • High-friction tires for short-field landings
Gear Specs
SUSPENSION
Strut Length

1.2 – 3.5 Meters

Adjustable

Suspension

Hydraulic Dampers

Variable Rate

Tire Grip

High-Friction

All-Weather

Retraction

Electric Motor

2.5s Cycle

Max Load Capacity45,000 kg

Start building your aircraft today

Access our full library of 1000+ parts and start designing your next flight project.

Aerodynamic Simulation Engine

Real-Time Telemetry & Flight Dynamics

Every part in your aircraft calculates its own airflow vectors, pressure differentials, and structural loads 60 times per second. Adjust test parameters below to see how our solver handles live aerodynamic shifts.

CFD Airflow & Pressure

Surface stream vectors & stall boundary detection

ATTACHED FLOW
P_DIFF: 13.9 kPa
Foil Profile:
Angle of Attack (AoA)+6 deg
Lift (C_L)
0.94
Crit Alpha
15.2 deg
Bound Sep
12%
CoM & CoL Dynamic Stability

Static margin, pitch authority & trim state

CALC: V-TAIL
NOSE (0% MAC)TAIL (100% MAC)
CoM
CoL
Pitch Status:Neutral (Agile Fly-By-Wire)
Fuel Load & Ballast Shift45% AFT
Static Margin
1.5%
CoM Position
48.5%
Damping Ratio
0.71 ζ
Drag Polar Resolution

Parasitic vs induced drag split & wave drag rise

POLAR: CD0 + K(CL^2)
Total Drag Coeff (C_D):
0.064
Induced Drag: 0.046Parasitic Drag: 0.018
L/D Efficiency Ratio:14.7 : 1
High angles of attack increase vortex roll-up, multiplying induced drag. As velocity enters transonic bands (Mach > 0.9), wave drag sharply increases parasite resistance.
Wetted Area
34.2 m²
Oswald Eff (e)
0.82
Wave Drag (C_Dw)
0.000
Mach Scaling & Thrust

Compressibility regimes & power-to-weight metrics

TRANSONIC
true Airspeed
1041 km/h
Dynamic Q
51.2 kPa
Mach RegimeM 0.85
Velocity Simulator (Mach)M 0.85
Thrust Req.
10 kN
T/W Ratio
1.35
Shock Angle
N/A

60Hz Deterministic Physics Core

Complex sub-grid vortices, structural flex, and supersonic shockwaves calculated without performance drops.

EDITION MATRIX

Sandbox Edition Comparison

Compare the free sandbox experience with our advanced engineering edition featuring wind-tunnel telemetry and custom scripting.

Capability Vector
ENGINEERING
PRO
Standard
Basic
Total Part Count
Component Library
1000+ Parts
Full library access
100 Parts
Basic kit only
50 Parts
Starter set only
Aerodynamic Fidelity
Simulation Engine
High-Mach CFD
Real-time telemetry
Standard Physics
Simplified drag
Basic Arcade
No lift curves
Telemetry Export
Data & Export
Full Data Export
CSV & JSON formats
Limited Export
Image only
No Export
View only
Custom Scripting
Automation
Full Scripting
Lua & Python API
Presets Only
No custom code
null
Static behavior
Build Complexity
Workspace
Unlimited Parts
No build limits
500 Parts
Moderate limit
100 Parts
Strict limit

Unlimited Design Freedom

Build complex aircraft with over 1000+ parts and advanced physics simulation.

Advanced CFD

Simulate airflow and lift vectors with high-precision computational fluid dynamics.

Telemetry Export

Export flight data and wind-tunnel results for external analysis and optimization.

Custom Scripting

Program custom flight controllers and engine management systems with our API.

AEROSAND is an immersive plane sandbox with 1000+ parts. Design, assemble, and test virtual aircraft with realistic physics.

Physics VerifiedCFD
Engine v2.4.0 Stable

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