I Class Rocket Motor

Cesaroni I360

Cesaroni Technology
Unknown
Ø 38mm
Total Impulse
625.5Ns
Burn Time
1.77s
Avg Thrust
360.0N
Max Thrust
555.5N

Thrust Profile (N)

1.77s Burn Window

Engineered by Cesaroni Technology, the I360 is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 625.5 Ns over a 1.77 second burn window.

With an average thrust of 360.0 N and a peak of 555.5 N, it features a regressive thrust curve optimal for general sport flying.

Technical Specifications

Tripoli Rocketry Association, Inc.
Diameter 38 mm
Length 360 mm
Hardware Pro38-5G
Delays (s) P
Specific Impulse 190.6 s
Peak Thrust 555.5 N
Peak Time T+ 0.08s
T/W Ratio —
Propellant Standard
Profile regressive
Type reload
Sparky No
Mass Budget Unavailable
Live Sizing
Flight Envelope

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Comparable I-Class Alternatives

I235WC

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I200W

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I180W

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I385F

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I223GT

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I161W

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