Total Impulse
113.7Ns
Burn Time
3.06s
Avg Thrust
37.2N
Max Thrust
66.8N
Thrust Profile (N)
3.06s Burn WindowEngineered by Public Missiles, Ltd., the G40W is a 29mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 113.7 Ns over a 3.06 second burn window.
With an average thrust of 37.2 N and a peak of 66.8 N, it features a regressive thrust curve optimal for general sport flying.
Technical Specifications
National Association of RocketryDiameter 29 mm
Length 124 mm
Hardware SU 29x124
Delays (s) 4,7
Specific Impulse 185.8 s
Peak Thrust 66.48 N
Peak Time T+ 0.037s
T/W Ratio —
Propellant Standard
Profile regressive
Type SU
Sparky No
Mass Budget Unavailable
Live Sizing
Flight Envelope
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