N Class Rocket Motor

Cesaroni 15227N2501-P

Cesaroni Technology
White
Ø 98mm
Total Impulse
15227.2Ns
Burn Time
6.09s
Avg Thrust
2501.8N
Max Thrust
3892.3N

Thrust Profile (N)

6.09s Burn Window

Engineered by Cesaroni Technology, the 15227N2501-P is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official N-class motor, it delivers a total impulse of 15227.2 Ns over a 6.09 second burn window.

With an average thrust of 2501.8 N and a peak of 3892.3 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 98 mm
Length 1010 mm
Hardware Pro98-6G
Delays (s) P
Specific Impulse 182.7 s
Peak Thrust 3488.42 N
Peak Time T+ 0.141s
T/W Ratio 19.16
Propellant White
Profile regressive
Type reload
Sparky No

Mass Budget

13308g Total
Casing (Dry)
4812.0g
36.2%
Propellant
8496.0g
63.8%
Live Sizing
Flight Envelope

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