NYX‑1

This model rocket is built around a mathematically defined ogive forebody. I chose it for its favourable subsonic pressure‑distribution characteristics and reduced form drag. The airframe geometry follows standard slender‑body design conventions. It maintains a consistent fineness ratio and smooth axial contouring to minimise boundary‑layer disturbances. The three‑fin empennage uses equal angular spacing and matched planform geometry. This provides passive static stability through predictable centre‑of‑pressure behaviour. The configuration reflects conventional low‑Reynolds‑number aerodynamic practice with clean surfaces and symmetric mass distribution. It prioritises stable, low‑drag flight dynamics, and was built with the Tsiolkovsky rocket equation in mind. Inspired by monocoques, i designed this model to be printed in one piece (might have to scale based on printer), which gives it superior strength to weight ratio, allowing it to handle the tortional and compressional forces of fl