Thrust Profile (N)
2.44s Burn WindowEngineered by AeroTech, the G55 is a 24mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 119.6 Ns over a 2.44 second burn window.
With an average thrust of 49.0 N and a peak of 84.7 N, it features a regressive thrust curve optimal for general sport flying.
Technical Specifications
National Association of RocketryDiameter 24 mm
Length 177 mm
Hardware SU 24x177
Delays (s) 5,6,7,8,9,10,11,13,15
Specific Impulse 195 s
Peak Thrust 84.65 N
Peak Time T+ 0.014s
T/W Ratio —
Propellant Standard
Profile regressive
Type SU
Sparky No
Mass Budget Unavailable
Live Sizing
Flight Envelope
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