Abstract

A dual-mode use Solid Controlled and Hybrid Rocket Engine, in the form of a cord/filament, of variable length, and single or multiple diameters, or shapes, coaxially packaged or comprising at least one, or more, canister-built common use bobbin-propellant housing(s), and at least one, or more, common use rocket engine combustion chamber(s), control feeding(s), and safety feature hardware, for modular-interchangeable space vehicle architectures, built-in variable performance feature-ability, for novel general propulsion uses.

IPC Classes  ?

• F02K 9/10 - Shape or structure of solid propellant charges
• F02K 9/24 - Charging rocket engines with solid propellantsMethods or apparatus specially adapted for working solid propellant charges
• F02K 9/72 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant thereforControl thereof using liquid and solid propellants, i.e. hybrid rocket-engine plants
• B64G 1/40 - Arrangements or adaptations of propulsion systems