L Class Rocket Motor

Cesaroni 3683L851-P

Cesaroni Technology
White
Ø 75mm
Total Impulse
3683.2Ns
Burn Time
4.34s
Avg Thrust
849.1N
Max Thrust
989.9N

Thrust Profile (N)

4.34s Burn Window

Engineered by Cesaroni Technology, the 3683L851-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 3683.2 Ns over a 4.34 second burn window.

With an average thrust of 849.1 N and a peak of 989.9 N, it features a dual-peak thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the White 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 177.9 s
Peak Thrust 980.11 N
Peak Time T+ 1.824s
T/W Ratio 22.84
Propellant White
Profile dual-peak
Type reload
Sparky No

Mass Budget

3789g Total
Casing (Dry)
1679.0g
44.3%
Propellant
2110.0g
55.7%
Live Sizing
Flight Envelope

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