I Class Rocket Motor

Cesaroni 396I195-16A

Cesaroni Technology
Red Lightning
Ø 38mm
Total Impulse
369.2Ns
Burn Time
2.02s
Avg Thrust
196.0N
Max Thrust
241.5N

Thrust Profile (N)

2.02s Burn Window

Engineered by Cesaroni Technology, the 396I195-16A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 369.2 Ns over a 2.02 second burn window.

With an average thrust of 196.0 N and a peak of 241.5 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Red Lightning propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 38 mm
Length 245 mm
Hardware Pro38-3G
Delays (s) 7,9,11,13,16
Specific Impulse 183.7 s
Peak Thrust 235.42 N
Peak Time T+ 0.3s
T/W Ratio 47.91
Propellant Red Lightning
Profile dual-peak
Type reload
Sparky No

Mass Budget

417g Total
Casing (Dry)
212.1g
50.9%
Propellant
204.9g
49.1%
Live Sizing
Flight Envelope

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