M Class Rocket Motor

Cesaroni 7312M4770-P

Total Impulse
7312.4Ns
Burn Time
1.53s
Avg Thrust
4770.2N
Max Thrust
6053.4N

Thrust Profile (N)

1.53s Burn Window

Engineered by Cesaroni Technology, the 7312M4770-P is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 7312.4 Ns over a 1.53 second burn window.

With an average thrust of 4770.2 N and a peak of 6053.4 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Vmax propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 98 mm
Length 548 mm
Hardware Pro98-3G
Delays (s) P
Specific Impulse 208.3 s
Peak Thrust 5854.33 N
Peak Time T+ 0.04s
T/W Ratio 74.77
Propellant Vmax
Profile dual-peak
Type reload
Sparky No

Mass Budget

6503g Total
Casing (Dry)
2924.0g
45.0%
Propellant
3579.0g
55.0%
Live Sizing
Flight Envelope

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