Total Impulse
382.0Ns
Burn Time
1.00s
Avg Thrust
280.0N
Max Thrust
334.0N
Thrust Profile (N)
1.00s Burn WindowEngineered by Kosdon by AeroTech, the I280F is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 382.0 Ns over a 1.00 second burn window.
With an average thrust of 280.0 N and a peak of 334.0 N, it features a neutral thrust curve optimal for general sport flying.
Technical Specifications
Tripoli Rocketry Association, Inc.Diameter 38 mm
Length 314 mm
Hardware 38-390
Delays (s) P
Specific Impulse 214 s
Peak Thrust 330.31 N
Peak Time T+ 0.735s
T/W Ratio —
Propellant Standard
Profile neutral
Type reload
Sparky No
Mass Budget Unavailable
Live Sizing
Flight Envelope
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