L Class Rocket Motor

Cesaroni 3300L3200-P

Total Impulse
3300.3Ns
Burn Time
1.03s
Avg Thrust
3209.4N
Max Thrust
3723.0N

Thrust Profile (N)

1.03s Burn Window

Engineered by Cesaroni Technology, the 3300L3200-P is a 75mm solid rocket motor designed for extreme high-power rocketry. As an official L-class motor, it delivers a total impulse of 3300.3 Ns over a 1.03 second burn window.

With an average thrust of 3209.4 N and a peak of 3723.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Vmax propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 75 mm
Length 486 mm
Hardware Pro75-3G
Delays (s) P
Specific Impulse 216.3 s
Peak Thrust 3711.92 N
Peak Time T+ 0.524s
T/W Ratio 100.24
Propellant Vmax
Profile dual-peak
Type reload
Sparky No

Mass Budget

3263.7g Total
Casing (Dry)
1708.7g
52.4%
Propellant
1555.0g
47.6%
Live Sizing
Flight Envelope

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