K Class Rocket Motor

Cesaroni 2398K590-15A

Cesaroni Technology
Classic/Dual Thrust
Ø 54mm
Total Impulse
2397.6Ns
Burn Time
4.06s
Avg Thrust
590.5N
Max Thrust
1497.6N

Thrust Profile (N)

4.06s Burn Window

Engineered by Cesaroni Technology, the 2398K590-15A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2397.6 Ns over a 4.06 second burn window.

With an average thrust of 590.5 N and a peak of 1497.6 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Classic/Dual Thrust propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 54 mm
Length 572 mm
Hardware Pro54-6G
Delays (s) 6,7,8,9,10,11,12,13,14,15
Specific Impulse 209.1 s
Peak Thrust 1812.1 N
Peak Time T+ 0.04s
T/W Ratio 30.19
Propellant Classic/Dual Thrust
Profile regressive
Type reload
Sparky No

Mass Budget

1994g Total
Casing (Dry)
825.0g
41.4%
Propellant
1169.0g
58.6%
Live Sizing
Flight Envelope

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