I Class Rocket Motor

AeroTech I600R

AeroTech
Redline
Ø 38mm
Total Impulse
597.3Ns
Burn Time
1.09s
Avg Thrust
612.0N
Max Thrust
811.7N

Thrust Profile (N)

1.09s Burn Window

Engineered by AeroTech, the I600R is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 597.3 Ns over a 1.09 second burn window.

With an average thrust of 612.0 N and a peak of 811.7 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Redline propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Tripoli Rocketry Association, Inc.
Diameter 38 mm
Length 345.4 mm
Hardware RMS-38/720
Delays (s) 4,6,8,10
Specific Impulse 187.9 s
Peak Thrust 817.75 N
Peak Time T+ 0.046s
T/W Ratio 103.63
Propellant Redline
Profile regressive
Type reload
Sparky No

Mass Budget

602g Total
Casing (Dry)
278.0g
46.2%
Propellant
324.0g
53.8%
Live Sizing
Flight Envelope

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Comparable I-Class Alternatives

I235WC

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No Curve Data
Total: 324 Ns
Ø 38mm

I200W

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regressive
Total: 325 Ns
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I180W

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dual-peak
Total: 326 Ns
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I385F

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No Curve Data
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I223GT

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neutral
Total: 328 Ns
Ø 38mm

I161W

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dual-peak
Total: 329 Ns
Ø 38mm
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