首页>
外国专利>
LAUNCHER STAGE COMPRISING A TEMPORARY SUPPORT STRUCTURE FOR TEMPORARILY SUPPORTING NOZZLE SECTIONS ALLOWING ACCESS TO THE CORE OF THE ENGINE
LAUNCHER STAGE COMPRISING A TEMPORARY SUPPORT STRUCTURE FOR TEMPORARILY SUPPORTING NOZZLE SECTIONS ALLOWING ACCESS TO THE CORE OF THE ENGINE
展开▼
机译:包含临时支持结构的发射器阶段,用于临时支持可访问引擎核心的喷嘴部分
展开▼
页面导航
摘要
著录项
相似文献
摘要
A stage of a space launcher including an engine core, a tank secured above the engine core, and a nozzle including a first deployable nozzle section secured below the engine core, the nozzle further including a second and a third section configured to be situated extending from each other when the nozzle is in a deployed propulsion configuration. The stage further includes a structure for temporarily supporting nozzle sections mounted on the tank, configured to change the nozzle to a configuration for accessing the engine core wherein the nozzle sections are inserted into each other, with the third section bearing against a lower support of the temporary structure.
展开▼