M Class Rocket Motor

Cesaroni 6819M1540-P

Total Impulse
6819.4Ns
Burn Time
4.44s
Avg Thrust
1537.0N
Max Thrust
2328.8N

Thrust Profile (N)

4.44s Burn Window

Engineered by Cesaroni Technology, the 6819M1540-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 6819.4 Ns over a 4.44 second burn window.

With an average thrust of 1537.0 N and a peak of 2328.8 N, it features a dual-peak 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 757 mm
Hardware Pro75-5G
Delays (s) P
Specific Impulse 191.8 s
Peak Thrust 2400 N
Peak Time T+ 0.08s
T/W Ratio 26.53
Propellant Imax
Profile dual-peak
Type reload
Sparky No

Mass Budget

5906g Total
Casing (Dry)
2281.6g
38.6%
Propellant
3624.4g
61.4%
Live Sizing
Flight Envelope

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