Total Impulse
633.8Ns
Burn Time
2.10s
Avg Thrust
310.0N
Max Thrust
473.9N
Thrust Profile (N)
2.10s Burn WindowEngineered by Kosdon by AeroTech, the I310S is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 633.8 Ns over a 2.10 second burn window.
With an average thrust of 310.0 N and a peak of 473.9 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 204.3 s
Peak Thrust 351.94 N
Peak Time T+ 1.146s
T/W Ratio —
Propellant Standard
Profile dual-peak
Type reload
Sparky No
Mass Budget Unavailable
Live Sizing
Flight Envelope
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