Thrust Profile (N)
1.56s Burn WindowEngineered by Animal Motor Works, the 1951K1250-P is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official K-class motor, it delivers a total impulse of 1950.9 Ns over a 1.56 second burn window.
With an average thrust of 1251.9 N and a peak of 1660.9 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Wild Wolf propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
1815g TotalDesign wings in your spreadsheet
AeroSheet loads airfoils directly into Google Sheets. Polars, 3D splines, Fusion 360 export, without leaving your spreadsheet.
1176K1720-P
AMW
1281K360-13A
Cesaroni
K456DM
AeroTech
835CC125J-K240
Hypertek
SK-54-1750
AMW
K400C
AeroTech
Need a custom engineering simulator?
The 3D engine on this page is built by Veenie Aerospace. We build bespoke, browser-native digital twins, aerodynamic simulators, and AI physics tools for UAV startups and defense contractors.