K Class Rocket Motor

Cesaroni 2014K1200-16A

Cesaroni Technology
White Thunder
Ø 54mm
Total Impulse
2014.0Ns
Burn Time
1.69s
Avg Thrust
1194.0N
Max Thrust
1363.9N

Thrust Profile (N)

1.69s Burn Window

Engineered by Cesaroni Technology, the 2014K1200-16A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2014.0 Ns over a 1.69 second burn window.

With an average thrust of 1194.0 N and a peak of 1363.9 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the White Thunder propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 54 mm
Length 404 mm
Hardware Pro54-5G
Delays (s) 6,7,8,9,10,11,12,13,14,15,16
Specific Impulse 213.9 s
Peak Thrust 1369.46 N
Peak Time T+ 0.02s
T/W Ratio 74.58
Propellant White Thunder
Profile regressive
Type reload
Sparky No

Mass Budget

1631.9g Total
Casing (Dry)
671.9g
41.2%
Propellant
960.0g
58.8%
Live Sizing
Flight Envelope

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Comparable K-Class Alternatives

1176K1720-P

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1281K360-13A

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K456DM

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835CC125J-K240

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SK-54-1750

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K400C

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regressive
Total: 1304 Ns
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