Thrust Profile (N)
2.70s Burn WindowEngineered by AeroTech, the HP-L1000W is a 54mm solid rocket motor designed for extreme high-power rocketry. As an official L-class motor, it delivers a total impulse of 2714.0 Ns over a 2.70 second burn window.
With an average thrust of 1000.0 N and a peak of 1261.0 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the White Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
2194g TotalDesign wings in your spreadsheet
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