K Class Rocket Motor

Cesaroni 2021K261-P

Cesaroni Technology
White
Ø 54mm
Total Impulse
2020.9Ns
Burn Time
7.78s
Avg Thrust
259.8N
Max Thrust
370.1N

Thrust Profile (N)

7.78s Burn Window

Engineered by Cesaroni Technology, the 2021K261-P is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2020.9 Ns over a 7.78 second burn window.

With an average thrust of 259.8 N and a peak of 370.1 N, it features a dual-peak 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 54 mm
Length 488 mm
Hardware Pro54-5G
Delays (s) P
Specific Impulse 178.8 s
Peak Thrust 359.35 N
Peak Time T+ 0.85s
T/W Ratio 13.71
Propellant White
Profile dual-peak
Type reload
Sparky No

Mass Budget

1931.7g Total
Casing (Dry)
779.8g
40.4%
Propellant
1151.9g
59.6%
Live Sizing
Flight Envelope

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