Thrust Profile (N)
1.34s Burn WindowEngineered by AeroTech, the K1999N is a 98mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 2540.0 Ns over a 1.34 second burn window.
With an average thrust of 1887.4 N and a peak of 2159.6 N, it features a dual-peak 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.Mass Budget
2989g TotalDesign wings in your spreadsheet
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