L Class Rocket Motor

Cesaroni 2856L910-P

Cesaroni Technology
C-Star
Ø 75mm
Total Impulse
2856.1Ns
Burn Time
3.15s
Avg Thrust
907.1N
Max Thrust
1086.1N

Thrust Profile (N)

3.15s Burn Window

Engineered by Cesaroni Technology, the 2856L910-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 2856.1 Ns over a 3.15 second burn window.

With an average thrust of 907.1 N and a peak of 1086.1 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the C-Star propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 75 mm
Length 350 mm
Hardware Pro75-2G
Delays (s) P
Specific Impulse 229.2 s
Peak Thrust 1047.55 N
Peak Time T+ 1.221s
T/W Ratio 35.35
Propellant C-Star
Profile neutral
Type reload
Sparky No

Mass Budget

2615.8g Total
Casing (Dry)
1345.8g
51.4%
Propellant
1270.0g
48.6%
Live Sizing
Flight Envelope

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