solid-rocket-motor

An open-source internal ballistics simulator for rocket motor experimenters

Burnback analysis for solid propellant rockets, with Time Marching Method (Mirror for CI)

3D burnback analysis for solid propellant rockets, with Time Marching Method (Mirror for CI)

A 100 kN solid rocket motor: ballistic design, thermal protections and a reusable water cooling jacket.

Diseño preliminar de un motor cohete de combustible sólido (APCP) para 11 km de apogeo, banco de ensayos vertical instrumentado (20 kN) y sistema de ignición compuesto.

Solid rocket motor burnback and ballistics, calibrated to a certified static test and validated against a measured flight (apogee within 0.5%). Sobol analysis of what drives flight dispersion.

Rocket Simulation Project uses RocketPy to simulate rocket performance with Cesaroni M1670 motor data. It features thrust-time curves, drag analysis (power-on/off), and Google Earth trajectory visualization. The goal is to provide a reproducible workflow integrating experimental data and advanced simulation tools.

Reverse-design a 2D solid-propellant rocket grain from a target chamber-pressure curve, by evolving a neural network whose level set is the grain shape. Python reimplementation of Li et al., Aerospace 2022, 9(10), 552.

Construção de programa em python baseado na planilha casing de Richard Nakka.

Integrated design, ballistics, thermal analysis, and feed‑system sizing of a 100 kN class solid rocket motor (AP/HTPB) with MDN250 case, EPDM/CCF/KP TBC, and active water cooling.

REF·DB — learning-first reference for solid rocket motor and mechanical design engineering