Rocket Designer

Build your paper rocket visually — real-time stability analysis, mass budget, and Barrowman CP calculation

Live Rocket Visualization

▼
View from nose (looking aft)
Paper body
Packing tape gloss
Electrical tape
Fins
CG center of gravity
CP center of pressure

Body Configuration

▼

Rocket is rolled around this tube

11.5"
6"24"
Computed Properties
Inner diameter (fits tube)0.840"
Wall thickness -
Outer diameter -
Paper mass -
Packing tape mass -

Nose Cone

▼

Paper cone taped on with electrical tape. No cone = great for little kids!

6.00"
2" (short)6" (tall)
1
010
0 g
0 g30 g (scrap paper & tape)
Computed Properties
Nose Cd contribution -
Cone height -
Cone half-angle -
Nose mass (total) -

Fin Configuration

▼
1.8"
0.5"6"
0.5"
0"4"
0.7"
0.1"4"
60°
0°80°
3.0°
0° no spin30° max spin
0.0"
flush with tail11" (near nose)
Computed Properties
Per-fin area -
Per-fin mass -
Total fin mass -
Estimated spin -

Forward Fins (Canards)

▼
Forward fins (canards) shift CP forward, reducing stability margin. Use sparingly - they can make the rocket less stable but more maneuverable. Not recommended for beginners.

Electrical Tape (Balance Weight)

▼
7
110
0%
Front of tubeTail end
Computed
Tape mass added -
Tape position (from front of tube) -
Electrical tape near the front of the body tube shifts CG forward, increasing stability margin. More wraps = more mass = greater nose-heavy shift. Position is measured along the body tube only (0% = front of tube, regardless of nose cone).

Mass Budget

▼
Total Rocket Mass
-
In ounces
-

Stability Analysis (Barrowman Method)

▼
- Center of Gravity from nose
- Center of Pressure from nose
CG (blue) and CP (red) position along rocket length:
CG
CP
Nose tip (0")Tail end
Stability Margin
-
calibers (diameters)
Calculating…
Stability range
-
<0.5 unstable 0.5-1 marginal 1-3 stable >4 overstable
Stability Advice
Adjust parameters to see stability tips.
Barrowman Component Breakdown
Nose normal force coeff (Cn) -
Nose CP from nose tip -
Fin normal force coeff (Cn) -
Fin CP from nose tip -
Total Cn -
Fin-body interference Kfb -

Aerodynamic Properties

▼
-
Total Drag Cd
-
Est. Spin (RPM)
-
Reynolds No.
-
Nose Drag Cd
-
Body Friction Cd
-
Fin Drag Cd
Canted fins create gyroscopic spin stabilization like a rifled bullet.

Design Templates

▼
🎯
The Dart
Minimal drag, heavy nose
🎈
The Floater
Max hang time
🌀
The Spinner
High spin stabilization
📏
Distance King
Max horizontal range
🏢
Sky Scraper
Max altitude

Save / Load / Export

▼
Save Current Design
Saved Designs
No saved designs yet.