M Class Rocket Motor

Cesaroni 6251M1400-P

Cesaroni Technology
Classic
Ø 75mm
Total Impulse
6251.0Ns
Burn Time
4.47s
Avg Thrust
1398.0N
Max Thrust
2291.8N

Thrust Profile (N)

4.47s Burn Window

Engineered by Cesaroni Technology, the 6251M1400-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 6251.0 Ns over a 4.47 second burn window.

With an average thrust of 1398.0 N and a peak of 2291.8 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 75 mm
Length 757 mm
Hardware Pro75-5G
Delays (s) P
Specific Impulse 213 s
Peak Thrust 2291.75 N
Peak Time T+ 0.11s
T/W Ratio 26.88
Propellant Classic
Profile regressive
Type reload
Sparky No

Mass Budget

5302g Total
Casing (Dry)
2310.0g
43.6%
Propellant
2992.0g
56.4%
Live Sizing
Flight Envelope

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