I Class Rocket Motor

AeroTech I599N

AeroTech
Warp 9
Ø 54mm
Total Impulse
404.9Ns
Burn Time
0.60s
Avg Thrust
667.8N
Max Thrust
763.5N

Thrust Profile (N)

0.60s Burn Window

Engineered by AeroTech, the I599N is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official I-class motor, it delivers a total impulse of 404.9 Ns over a 0.60 second burn window.

With an average thrust of 667.8 N and a peak of 763.5 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Warp 9 propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Tripoli Rocketry Association, Inc.
Diameter 54 mm
Length 156 mm
Hardware RMS-54/426
Delays (s) P
Specific Impulse 211.6 s
Peak Thrust 797.44 N
Peak Time T+ 0.017s
T/W Ratio 132.96
Propellant Warp 9
Profile regressive
Type reload
Sparky No

Mass Budget

512g Total
Casing (Dry)
317.0g
61.9%
Propellant
195.0g
38.1%
Live Sizing
Flight Envelope

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