M Class Rocket Motor

Cesaroni 5506M1230-P

Total Impulse
5506.5Ns
Burn Time
4.48s
Avg Thrust
1229.6N
Max Thrust
1586.6N

Thrust Profile (N)

4.48s Burn Window

Engineered by Cesaroni Technology, the 5506M1230-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 5506.5 Ns over a 4.48 second burn window.

With an average thrust of 1229.6 N and a peak of 1586.6 N, it features a neutral thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Imax 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 193.6 s
Peak Thrust 1507.12 N
Peak Time T+ 1.767s
T/W Ratio 25.88
Propellant Imax
Profile neutral
Type reload
Sparky No

Mass Budget

4844g Total
Casing (Dry)
1944.0g
40.1%
Propellant
2900.0g
59.9%
Live Sizing
Flight Envelope

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