GGDT Comparison Guide

Using Gas Gun Design Tool to validate pneumatic launcher calculations

Table of Contents

1. What is GGDT?

Gas Gun Design Tool (GGDT) is a simulation program developed by David Hall (D_Hall) for designing pneumatic cannons. It's considered the gold standard in the spudgun community for predicting pneumatic launcher performance.

Accuracy: GGDT typically outputs numbers within 5-10% of measured values when proper input parameters are used. The tool has been verified many times with actual testing.

What GGDT Models

What GGDT Does NOT Model

2. Installation

Download

GGDT is available from SpudFiles. The current version is 4.4 or 4.6.

Required Files

Place these files in the same folder:

Windows 7+: Right-click on ggdt.exe and select "Run as Administrator". You may also need to enable XP compatibility mode.

Linux Users

GGDT can run under Wine:

wine ggdt4.4.exe

3. Parameter Reference

Reservoir Data (Chamber)

Parameter Description Notes
Outer Diameter Outside diameter of chamber pipe Use pipe OD from specifications
Inner Diameter Diameter of any pipe running through chamber Set to 0 for most designs! Only non-zero for coaxial designs where barrel runs through chamber
Length Length of the pressure chamber Internal length, not including fittings
Pressure Operating pressure Gauge pressure (psig)
Gas Type Propellant gas Usually "Air"

Barrel Data

Parameter Description Notes
Bore Diameter Inside diameter of barrel Use pipe ID from specifications
Length Barrel length From valve seat to muzzle

Projectile Data

Parameter Description Notes
Mass Weight of projectile In grams
Diameter Projectile diameter Affects blow-by calculation
Friction Friction force Typically 0-5 PSI equivalent for golf balls

Valve Data

Parameter Description Notes
Valve Type Configuration of valve Chamber sealing pilot, Barrel sealing pilot, Burst disk, Hammer, Generic
Seat Diameter Effective opening diameter Determines flow area
Flow Coefficient Valve flow restriction % of ideal flow (not manufacturer Cv!)
Opening Time Time to fully open In milliseconds - critical parameter!
Dwell Time Time valve stays open Set to 999 for valves that stay open
Dead Volume Volume between projectile base and valve In cubic inches

4. Golf Ball Launcher Walkthrough

Real-World Test Data (Your Launcher)

ParameterValue
Barrel TypeSDR26 1.5" (ID = 1.754")
Barrel Length30 inches
Chamber2" x 40" (ID = 2.067")
Pressure25 psi
Launch Angle40 degrees
ProjectileGolf ball (45.93g, 42.67mm / 1.68")
Measured Range~25 yards (75 feet)
At 125 psiClose to 200 yards

1Reservoir Data

For a 2" Schedule 40 chamber (40 inches long):

GGDT Field Value to Enter Why
Outer Diameter 2.375 in 2" Sch40 OD
Inner Diameter 0 in Not a coaxial design
Length 40 in Chamber length
Initial Pressure 25 psig Your test pressure
Gas Air Standard propellant
Chamber Volume: ~134 cubic inches
V = π × (2.067/2)² × 40 = 134.2 in³

2Barrel Data

For SDR26 1.5" barrel (30 inches long):

GGDT Field Value to Enter Why
Bore Diameter 1.754 in SDR26 1.5" ID
Length 30 in Barrel length
Barrel Volume: ~72.5 cubic inches
V = π × (1.754/2)² × 30 = 72.5 in³

3Projectile Data

GGDT Field Value to Enter Why
Mass 45.93 g Standard golf ball mass
Diameter 1.68 in Golf ball = 42.67mm
Friction 0-2 psi Golf balls have low friction; some blow-by helps
Blow-by Gap: 1.754" - 1.68" = 0.074" total gap
Gap Ratio = (barrel area - ball area) / ball area = ~8.9%
This is a loose fit with significant blow-by!

4Valve Data

For QEV (Quick Exhaust Valve)

GGDT Field 3/4" QEV 1/2" QEV
Valve Type Barrel Sealing Pilot Barrel Sealing Pilot
Seat Diameter 1.25 in 0.75 in
Flow Coefficient 45-60% 45%
Opening Time 2-5 ms 2-3 ms
Dwell Time 999 ms 999 ms
Dead Volume 1.178 in³ 0.5 in³
Piston Diameter 1.75 in 1.0 in
Piston Mass 8.3 g 4 g
Pilot Volume 0.98 in³ 0.5 in³

For Sprinkler Valve (Modified)

GGDT Field 1" Sprinkler (modded) 3/4" Sprinkler
Valve Type Generic Generic
Seat Diameter 1.0 in 0.75 in
Flow Coefficient 35-45% 35%
Opening Time 15-30 ms 20-40 ms
Dwell Time 999 ms 999 ms
Dead Volume 2-4 in³ 1-2 in³
Critical Note: Sprinkler valves are 50-60ms to open with stock solenoid. Modified with blowgun pilot: 15-30ms. This slow opening drastically reduces performance compared to QEV!

5Run Simulation

After entering all values, click "Calculate" or "Run" in GGDT.

Key Output Values to Compare:

Expected GGDT Output (approximate):
At 25 psi with SDR26 barrel and QEV, expect ~80-120 fps muzzle velocity.
At 125 psi, expect ~300-400 fps.

5. Valve Data Reference

Valve Opening Times

Valve Type Opening Time Performance Impact
QEV (1/2" - 1") 1-5 ms Excellent - snap-open design
Custom Piston Valve 1-5 ms Excellent if well designed
Spring Ball Valve 20-30 ms Good for slow projectiles
Hand Ball Valve 100+ ms Poor - significant loss
Sprinkler (stock) 50-60 ms Poor
Sprinkler (modded) 15-30 ms Moderate

Why Opening Time Matters

For a projectile with 500 fps exit velocity in a 36" barrel, transit time is only ~12 milliseconds. If your valve takes 30ms to open, the projectile exits before the valve is fully open!

GGDT Comparison (same launcher):
30ms valve: 172 m/s, 295.8 J
Fast piston valve: 236.7 m/s, 560.2 J
Nearly 2x the energy just from valve speed!

Flow Coefficient (Cv) Estimation

Use this formula for quick Cv estimates:

Cv = K × D² (where D = seat diameter in cm)
Valve Type K Value Example
Sprinkler / Ball Valve K = 1 1" valve → Cv ≈ 6.5
Piston / QEV K = 2 1/2" QEV → Cv ≈ 3.4
Burst Disc K = 3 1" disc → Cv ≈ 19.5
Note: GGDT uses Flow Coefficient as a percentage (0-100%), not the actual Cv number from manufacturer datasheets!

6. Physics Equations Used

Basic Hand Calculation (D_Hall's Method)

For quick estimates without GGDT:

1. Exit Pressure (Isothermal Expansion)

Pexit = Pstart × Vchamber / (Vchamber + Vbarrel)

2. Muzzle Energy

E = (Pstart + Pexit) / 2 × Lbarrel × π/4 × Dbore²

3. Muzzle Velocity

v = √(2 × E / m)
Limitations of Basic Equations:
  • Assumes instant valve opening
  • Ignores blow-by around projectile
  • Ignores valve flow restriction
  • Uses isothermal instead of adiabatic expansion
  • Ignores friction
These simplifications can lead to 2-5x overestimation of actual performance!

More Accurate Model (What GGDT Does)

Adiabatic Expansion

Pexit = Pstart × (V1/V2)γ

Where γ = 1.4 for air (heat capacity ratio)

Work Done by Gas

W = P1V1/(γ-1) × [1 - (V1/V2)γ-1]

Valve Flow Restriction

Mass flow rate through valve is limited by:

Blow-by (Projectile Leakage)

Air escaping around projectile reduces effective pressure:

7. Experimental Validation Data

Your Golf Ball Launcher Data

Test Conditions Measured Result Notes
25 psi, 40° angle, 30" SDR26 barrel ~25 yards Plus ~25 yards roll
125 psi, similar setup ~200 yards Close but shy

Velocity Back-Calculation from Range

For a 40° launch angle and 25 yard (75 ft / 22.9m) range:

Range = v² × sin(2θ) / g
22.9 = v² × sin(80°) / 9.8
v ≈ 15.2 m/s ≈ 50 ft/s

This is a very rough estimate ignoring drag, but suggests muzzle velocity around 50-70 fps at 25 psi.

SpudFiles Community Data

Test Velocity Conditions
3/4" Sprinkler 388 fps 40 CI chamber, 5' CPVC, 100 PSI
1/2" QEV 517 fps Same setup - 33% higher!
4.5mm barrel (tight) 279 fps Lead BBs, 100 psi
5mm barrel (loose) 242 fps Same - 33% less energy from blow-by

8. Sources

Primary References

Academic References

Other Tools

Next Steps

  1. Download and install GGDT from SpudFiles
  2. Enter the golf ball launcher parameters from this guide
  3. Run simulation and note the predicted velocity
  4. Compare with our web calculator results
  5. Use GGDT's numbers to calibrate our physics model