N Class Rocket Motor

Cesaroni 12066N2200-P

Total Impulse
12066.0Ns
Burn Time
5.55s
Avg Thrust
2174.0N
Max Thrust
2879.0N

Thrust Profile (N)

5.55s Burn Window

Engineered by Cesaroni Technology, the 12066N2200-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 12066.0 Ns over a 5.55 second burn window.

With an average thrust of 2174.0 N and a peak of 2879.0 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Pink propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 98 mm
Length 1010 mm
Hardware Pro98-5G
Delays (s) P
Specific Impulse 200.9 s
Peak Thrust 2755.85 N
Peak Time T+ 0.033s
T/W Ratio 19.51
Propellant Pink
Profile regressive
Type reload
Sparky No

Mass Budget

11356g Total
Casing (Dry)
5234.0g
46.1%
Propellant
6122.0g
53.9%
Live Sizing
Flight Envelope

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