Total Impulse
634.3Ns
Burn Time
1.70s
Avg Thrust
370.0N
Max Thrust
539.2N
Thrust Profile (N)
1.70s Burn WindowEngineered by Kosdon by AeroTech, the I370F is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 634.3 Ns over a 1.70 second burn window.
With an average thrust of 370.0 N and a peak of 539.2 N, it features a dual-peak thrust curve optimal for general sport flying.
Technical Specifications
Tripoli Rocketry Association, Inc.Diameter 38 mm
Length 368 mm
Hardware AMW 38-640
Delays (s) P
Specific Impulse 204 s
Peak Thrust 447.33 N
Peak Time T+ 0.559s
T/W Ratio —
Propellant Standard
Profile dual-peak
Type reload
Sparky No
Mass Budget Unavailable
Live Sizing
Flight Envelope
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