Total Impulse
374.0Ns
Burn Time
2.00s
Avg Thrust
170.0N
Max Thrust
211.0N
Thrust Profile (N)
2.00s Burn WindowEngineered by Kosdon by AeroTech, the I170S is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 374.0 Ns over a 2.00 second burn window.
With an average thrust of 170.0 N and a peak of 211.0 N, it features a dual-peak 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 209.5 s
Peak Thrust 209.2 N
Peak Time T+ 0.88s
T/W Ratio —
Propellant Standard
Profile dual-peak
Type reload
Sparky No
Mass Budget Unavailable
Live Sizing
Flight Envelope
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