Total Impulse
722.0Ns
Burn Time
1.93s
Avg Thrust
405.0N
Max Thrust
518.0N
Thrust Profile (N)
1.93s Burn WindowEngineered by Kosdon by AeroTech, the J405S is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 722.0 Ns over a 1.93 second burn window.
With an average thrust of 405.0 N and a peak of 518.0 N, it features a neutral thrust curve optimal for general sport flying.
Technical Specifications
Tripoli Rocketry Association, Inc.Diameter 38 mm
Length 476 mm
Hardware 38-800
Delays (s) P
Specific Impulse 200.5 s
Peak Thrust 528.5 N
Peak Time T+ 0.009s
T/W Ratio —
Propellant Standard
Profile neutral
Type reload
Sparky No
Mass Budget Unavailable
Live Sizing
Flight Envelope
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