J Class Rocket Motor

Cesaroni 1195J295-16A

Cesaroni Technology
Classic
Ø 54mm
Total Impulse
1196.3Ns
Burn Time
4.00s
Avg Thrust
298.0N
Max Thrust
450.5N

Thrust Profile (N)

4.00s Burn Window

Engineered by Cesaroni Technology, the 1195J295-16A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1196.3 Ns over a 4.00 second burn window.

With an average thrust of 298.0 N and a peak of 450.5 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 54 mm
Length 320 mm
Hardware Pro54-3G
Delays (s) 6,7,8,9,10,11,12,13,14,15,16
Specific Impulse 205.3 s
Peak Thrust 450.52 N
Peak Time T+ 0.04s
T/W Ratio 27.15
Propellant Classic
Profile regressive
Type reload
Sparky No

Mass Budget

1119g Total
Casing (Dry)
525.0g
46.9%
Propellant
594.0g
53.1%
Live Sizing
Flight Envelope

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