Thrust Profile (N)
4.44s Burn WindowEngineered by AeroTech, the N4800T is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official N-class motor, it delivers a total impulse of 19361.0 Ns over a 4.44 second burn window.
With an average thrust of 4800.0 N and a peak of 6599.4 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Blue Thunder propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
14784g TotalDesign wings in your spreadsheet
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