Thrust Profile (N)
2.43s Burn WindowEngineered by AeroTech, the G75J is a 29mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 135.6 Ns over a 2.43 second burn window.
With an average thrust of 75.0 N and a peak of 70.3 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Blackjack propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Diameter 29 mm
Length 194 mm
Hardware RMS-29/180
Delays (s) 4,6,8,10
Specific Impulse 132.5 s
Peak Thrust 78.85 N
Peak Time T+ 1.197s
T/W Ratio 32.82
Propellant Blackjack
Profile dual-peak
Type reload
Sparky No
Mass Budget
232.96g TotalCasing (Dry)
128.7g
55.2%
Propellant
104.3g
44.8%
Live Sizing
Flight Envelope
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