Thrust Profile (N)
1.33s Burn WindowEngineered by AeroTech, the F39T is a 24mm solid rocket motor designed for model rocketry. As an official F-class motor, it delivers a total impulse of 49.7 Ns over a 1.33 second burn window.
With an average thrust of 37.3 N and a peak of 59.5 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Blue Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
National Association of RocketryDiameter 24 mm
Length 70 mm
Hardware RMS-24/40
Delays (s) 4,5,6,7,9
Specific Impulse 223 s
Peak Thrust 59.47 N
Peak Time T+ 0.079s
T/W Ratio 62.81
Propellant Blue Thunder
Profile regressive
Type reload
Sparky No
Mass Budget
60.6g TotalCasing (Dry)
37.9g
62.5%
Propellant
22.7g
37.5%
Live Sizing
Flight Envelope
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