Total Impulse
497.0Ns
Burn Time
2.72s
Avg Thrust
182.0N
Max Thrust
648.0N
Thrust Profile (N)
2.72s Burn WindowEngineered by Contrail Rockets, the I210-PVC is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 497.0 Ns over a 2.72 second burn window.
With an average thrust of 182.0 N and a peak of 648.0 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 922 mm
Hardware 38 36 M PVC (550CC)
Delays (s) P
Specific Impulse 405.3 s
Peak Thrust 468.96 N
Peak Time —
T/W Ratio 21.32
Propellant Standard
Profile regressive
Type hybrid
Sparky No
Mass Budget
870g TotalCasing (Dry)
745.0g
85.6%
Propellant
125.0g
14.4%
Live Sizing
Flight Envelope
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