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Lists the foundational assumptions for the calculation method.
Defines terms and concepts related to aerodynamic forces on rockets.
Explains the method of dividing the rocket into sections for analysis.
Discusses the importance of a common reference point for C.P. measurements.
Defines symbols and methods for measuring C.P. from different rocket sections.
Explains the meaning of subscripts used in aerodynamic force notation.
Lists sources used for theoretical derivation of equations.
Provides equations for calculating normal force and C.P. for different nose shapes.
Discusses C.P. calculations for less common nose cone shapes.
Provides equations for normal force and C.P. of conical shoulder sections.
Explains that forces on cylindrical bodies are often negligible.
Provides equations for normal force and C.P. of conical boattail sections.
Details how to simplify fin shapes and calculate forces.
Illustrates various fin shapes and their idealizations for analysis.
Explains how air flow interaction affects fin forces.
Shows how to combine results from different rocket sections.
Step-by-step instructions for calculating nose C.P. using equations.
Step-by-step instructions for calculating conical shoulder C.P. using charts.
Step-by-step instructions for calculating conical boattail C.P. using charts.
Step-by-step instructions for calculating fin C.P. using charts.
Step-by-step instructions for combining section results for total C.P.
Outlines initial steps and considerations for designing a stable rocket.
Details the process of applying equations to determine rocket stability.
Explains stability considerations for rockets with multiple stages.
Demonstrates calculations for the Javelin model using equations and charts.
Analyzes the Recruiter model using equations, charts, and stability checks.
Examines the two-stage Arcon-HI model using equations and charts.
Describes a practical method for determining C.G. by balancing.
Details how to calculate C.G. based on component weights and positions.
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