Total Impulse
826.0Ns
Burn Time
1.90s
Avg Thrust
360.0N
Max Thrust
828.0N
Thrust Profile (N)
1.90s Burn WindowEngineered by Cesaroni Technology, the J360 is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 826.0 Ns over a 1.90 second burn window.
With an average thrust of 360.0 N and a peak of 828.0 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration.
Technical Specifications
Tripoli Rocketry Association, Inc.Diameter 38 mm
Length 419 mm
Hardware Pro38-6G
Delays (s) P
Specific Impulse 203.8 s
Peak Thrust 618.9 N
Peak Time T+ 0.041s
T/W Ratio 51.75
Propellant Standard
Profile regressive
Type reload
Sparky No
Mass Budget
709.184g TotalCasing (Dry)
296.1g
41.8%
Propellant
413.1g
58.2%
Live Sizing
Flight Envelope
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