J Class Rocket Motor

Cesaroni 1016J360-15A

Cesaroni Technology
Skidmark
Ø 54mm
Total Impulse
1015.9Ns
Burn Time
2.80s
Avg Thrust
362.3N
Max Thrust
559.3N

Thrust Profile (N)

2.80s Burn Window

Engineered by Cesaroni Technology, the 1016J360-15A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1015.9 Ns over a 2.80 second burn window.

With an average thrust of 362.3 N and a peak of 559.3 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Skidmark propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Tripoli Rocketry Association, Inc.
Diameter 54 mm
Length 321 mm
Hardware Pro54-3G
Delays (s) 5,6,7,8,9,10,11,12,13,14,15
Specific Impulse 170.9 s
Peak Thrust 560.65 N
Peak Time T+ 0.017s
T/W Ratio 33.46
Propellant Skidmark
Profile regressive
Type reload
Sparky Yes

Mass Budget

1104g Total
Casing (Dry)
498.0g
45.1%
Propellant
606.0g
54.9%
Live Sizing
Flight Envelope

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