Total Impulse
100.0Ns
Burn Time
0.86s
Avg Thrust
130.0N
Max Thrust
706.0N
Thrust Profile (N)
0.86s Burn WindowEngineered by Contrail Rockets, the G130-PVC is a 38mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 100.0 Ns over a 0.86 second burn window.
With an average thrust of 130.0 N and a peak of 706.0 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 406 mm
Hardware 38 16 M PVC (140CC)
Delays (s) P
Specific Impulse 109.6 s
Peak Thrust 662.06 N
Peak Time —
T/W Ratio 25.68
Propellant Standard
Profile regressive
Type hybrid
Sparky No
Mass Budget
516g TotalCasing (Dry)
423.0g
82.0%
Propellant
93.0g
18.0%
Live Sizing
Flight Envelope
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