M Class Rocket Motor

Cesaroni 6162M1675-P

Total Impulse
6162.0Ns
Burn Time
3.68s
Avg Thrust
1674.1N
Max Thrust
2499.2N

Thrust Profile (N)

3.68s Burn Window

Engineered by Cesaroni Technology, the 6162M1675-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 6162.0 Ns over a 3.68 second burn window.

With an average thrust of 1674.1 N and a peak of 2499.2 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Pink 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 208.1 s
Peak Thrust 2073 N
Peak Time T+ 1.018s
T/W Ratio 32.67
Propellant Pink
Profile neutral
Type reload
Sparky No

Mass Budget

5223g Total
Casing (Dry)
2204.0g
42.2%
Propellant
3019.0g
57.8%
Live Sizing
Flight Envelope

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