Thrust Profile (N)
2.39s Burn WindowEngineered by AeroTech, the F26FJ is a 29mm solid rocket motor designed for model rocketry. As an official F-class motor, it delivers a total impulse of 62.2 Ns over a 2.39 second burn window.
With an average thrust of 26.0 N and a peak of 39.2 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Black Max propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
National Association of RocketryDiameter 29 mm
Length 98 mm
Hardware Single Use
Delays (s) 6,7,9
Specific Impulse 147.1 s
Peak Thrust 38.29 N
Peak Time T+ 0.041s
T/W Ratio 26.24
Propellant Black Max
Profile regressive
Type SU
Sparky No
Mass Budget
101g TotalCasing (Dry)
57.9g
57.3%
Propellant
43.1g
42.7%
Live Sizing
Flight Envelope
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