Total Impulse
737.0Ns
Burn Time
1.30s
Avg Thrust
605.0N
Max Thrust
882.0N
Thrust Profile (N)
1.30s Burn WindowEngineered by Kosdon by AeroTech, the J605F is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 737.0 Ns over a 1.30 second burn window.
With an average thrust of 605.0 N and a peak of 882.0 N, it features a regressive 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 204.7 s
Peak Thrust 886.34 N
Peak Time T+ 0.024s
T/W Ratio —
Propellant Standard
Profile regressive
Type reload
Sparky No
Mass Budget Unavailable
Live Sizing
Flight Envelope
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