Rocket power gas system with fuel and oxidant containers - has containers manufactured from materials, non reactive with fuel or oxidant

摘要

A power system for a rocket consists of a drive gas generator, containers for oxidant and fuel, a drive gas addition, distribution and injection system, a multiple burner chamber with attached sliding nozzles and a control block with programmer device. The oxidant and fuel containers are manufactured from materials inert to these substances and filled with drive gas components during the storage. The oxidant and/or fuel are separated from the container walls by flexible jackets or bladders and the floor of the oxidant and fuel containers are made from oxidant and fuel inert welded sections.