N Class Rocket Motor

Cesaroni 17613N2900-P

Cesaroni Technology
Classic
Ø 98mm
Total Impulse
17613.7Ns
Burn Time
6.14s
Avg Thrust
2867.5N
Max Thrust
4164.5N

Thrust Profile (N)

6.14s Burn Window

Engineered by Cesaroni Technology, the 17613N2900-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 17613.7 Ns over a 6.14 second burn window.

With an average thrust of 2867.5 N and a peak of 4164.5 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 98 mm
Length 1239 mm
Hardware Pro98-6GXL
Delays (s) P
Specific Impulse 212.5 s
Peak Thrust 4022.13 N
Peak Time T+ 0.122s
T/W Ratio 20.63
Propellant Classic
Profile regressive
Type reload
Sparky No

Mass Budget

14166g Total
Casing (Dry)
5717.0g
40.4%
Propellant
8449.0g
59.6%
Live Sizing
Flight Envelope

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