Total Impulse
110.5Ns
Burn Time
3.10s
Avg Thrust
37.0N
Max Thrust
68.0N
Thrust Profile (N)
3.10s Burn WindowEngineered by Ellis Mountain, the G37 is a 24mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 110.5 Ns over a 3.10 second burn window.
With an average thrust of 37.0 N and a peak of 68.0 N, it features a regressive thrust curve optimal for general sport flying.
Technical Specifications
Tripoli Rocketry Association, Inc.Diameter 24 mm
Length 181 mm
Hardware SU 24x181
Delays (s) 6,10,P
Specific Impulse 181.7 s
Peak Thrust 69.59 N
Peak Time T+ 0.023s
T/W Ratio —
Propellant Standard
Profile regressive
Type SU
Sparky No
Mass Budget Unavailable
Live Sizing
Flight Envelope
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