M Class Rocket Motor

Cesaroni 5604M1830-P

Cesaroni Technology
C-Star
Ø 75mm
Total Impulse
5603.7Ns
Burn Time
3.07s
Avg Thrust
1826.5N
Max Thrust
2342.3N

Thrust Profile (N)

3.07s Burn Window

Engineered by Cesaroni Technology, the 5604M1830-P is a 75mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 5603.7 Ns over a 3.07 second burn window.

With an average thrust of 1826.5 N and a peak of 2342.3 N, it features a dual-peak 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 621 mm
Hardware Pro75-4G
Delays (s) P
Specific Impulse 224.7 s
Peak Thrust 2300.79 N
Peak Time T+ 0.018s
T/W Ratio 41.16
Propellant C-Star
Profile dual-peak
Type reload
Sparky No

Mass Budget

4524g Total
Casing (Dry)
1982.0g
43.8%
Propellant
2542.0g
56.2%
Live Sizing
Flight Envelope

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