J Class Rocket Motor

Cesaroni 699J145-19A

Cesaroni Technology
Skidmark
Ø 54mm
Total Impulse
699.1Ns
Burn Time
4.87s
Avg Thrust
143.7N
Max Thrust
505.3N

Thrust Profile (N)

4.87s Burn Window

Engineered by Cesaroni Technology, the 699J145-19A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 699.1 Ns over a 4.87 second burn window.

With an average thrust of 143.7 N and a peak of 505.3 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Skidmark propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 54 mm
Length 236 mm
Hardware Pro54-2G
Delays (s) 9,10,11,12,13,14,15,16,17,18,19
Specific Impulse 170.9 s
Peak Thrust 498.17 N
Peak Time T+ 0.018s
T/W Ratio 17.5
Propellant Skidmark
Profile regressive
Type reload
Sparky Yes

Mass Budget

837g Total
Casing (Dry)
420.0g
50.2%
Propellant
417.0g
49.8%
Live Sizing
Flight Envelope

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