M Class Rocket Motor

Cesaroni 6268M1401-P

Cesaroni Technology
White
Ø 75mm
Total Impulse
6268.3Ns
Burn Time
4.49s
Avg Thrust
1396.1N
Max Thrust
1669.5N

Thrust Profile (N)

4.49s Burn Window

Engineered by Cesaroni Technology, the 6268M1401-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 6268.3 Ns over a 4.49 second burn window.

With an average thrust of 1396.1 N and a peak of 1669.5 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the White 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 182.1 s
Peak Thrust 1669 N
Peak Time T+ 0.079s
T/W Ratio 24.65
Propellant White
Profile regressive
Type reload
Sparky No

Mass Budget

5774g Total
Casing (Dry)
2266.0g
39.2%
Propellant
3508.0g
60.8%
Live Sizing
Flight Envelope

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