M Class Rocket Motor

Cesaroni 5472M2250-P

Cesaroni Technology
C-Star
Ø 75mm
Total Impulse
5472.2Ns
Burn Time
2.41s
Avg Thrust
2267.5N
Max Thrust
2960.2N

Thrust Profile (N)

2.41s Burn Window

Engineered by Cesaroni Technology, the 5472M2250-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 5472.2 Ns over a 2.41 second burn window.

With an average thrust of 2267.5 N and a peak of 2960.2 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 224.1 s
Peak Thrust 2663.17 N
Peak Time T+ 0.877s
T/W Ratio 52.35
Propellant C-Star
Profile dual-peak
Type reload
Sparky No

Mass Budget

4415g Total
Casing (Dry)
1926.0g
43.6%
Propellant
2489.0g
56.4%
Live Sizing
Flight Envelope

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