Thrust Profile (N)
5.40s Burn WindowEngineered by AeroTech, the N2220DM is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official N-class motor, it delivers a total impulse of 10657.0 Ns over a 5.40 second burn window.
With an average thrust of 2199.0 N and a peak of 4472.0 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the Dark Matter propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
11997g TotalDesign wings in your spreadsheet
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