Total Impulse
247.0Ns
Burn Time
1.70s
Avg Thrust
141.0N
Max Thrust
297.0N
Thrust Profile (N)
1.70s Burn WindowEngineered by Contrail Rockets, the H141-PVC is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 247.0 Ns over a 1.70 second burn window.
With an average thrust of 141.0 N and a peak of 297.0 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 508 mm
Hardware 38 20 S PVC (185CC)
Delays (s) P
Specific Impulse 201.4 s
Peak Thrust 265.51 N
Peak Time T+ 0.002s
T/W Ratio 23.49
Propellant Standard
Profile regressive
Type hybrid
Sparky No
Mass Budget
612g TotalCasing (Dry)
487.0g
79.6%
Propellant
125.0g
20.4%
Live Sizing
Flight Envelope
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Comparable H-Class Alternatives
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