STRUCTURAL ANALYSIS

Ejection System

Black powder charge sizing and shear pin design for reliable deployment.

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01

Black Powder Sizing

Design pressure for reliable separation:

Rocket TypeDesign Pressure
Model rockets5-10 psi
High-power rockets10-15 psi
Simplified Formula
mBP≈0.006×D2×Lm_{BP} \approx 0.006 \times D^2 \times L

Where D = diameter (inches), L = chamber length (inches), result in grams.

Ground Testing

Always ground test ejection charges before flight. Start with calculated amount and adjust based on actual separation force.
02

Shear Pin Design

Shear pins prevent premature separation while allowing controlled ejection:

Pin SizeMaterialShear Force (lbs)
2-56Nylon20-30
4-40Nylon35-45
2-56Delrin25-35
2-56PTFE15-20
Number of Pins
npins=FsepFshear×0.75n_{pins} = \frac{F_{sep}}{F_{shear} \times 0.75}
Use a safety factor of 0.7-0.8 (not > 1.0) to ensure pins break reliably. Minimum 2 pins to prevent pivoting.
03

Vent Holes

Prevent ascent pressurization that could cause premature separation:

1% Rule
Avent≈0.01×AcrossA_{vent} \approx 0.01 \times A_{cross}

Typical: 1/8" to 1/4" hole per bay. See the Vent Sizing page for detailed calculations.

SOURCES

References

Community Resources

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