I Class Rocket Motor

Cesaroni 601I350-16A

Cesaroni Technology
Smoky Sam
Ø 38mm
Total Impulse
601.0Ns
Burn Time
1.71s
Avg Thrust
352.1N
Max Thrust
399.7N

Thrust Profile (N)

1.71s Burn Window

Engineered by Cesaroni Technology, the 601I350-16A is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 601.0 Ns over a 1.71 second burn window.

With an average thrust of 352.1 N and a peak of 399.7 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Smoky Sam propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 38 mm
Length 360 mm
Hardware Pro38-5G
Delays (s) 7,9,11,13,16
Specific Impulse 148.2 s
Peak Thrust 399.74 N
Peak Time T+ 0.05s
T/W Ratio 45.9
Propellant Smoky Sam
Profile regressive
Type reload
Sparky No

Mass Budget

782g Total
Casing (Dry)
368.5g
47.1%
Propellant
413.5g
52.9%
Live Sizing
Flight Envelope

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