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Engine with a central spike for a space launcher

机译：具有用于太空发射器的中央尖头的发动机

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摘要

According to the present invention, the pointed end (11) of the central spike (7) consists of a deformable structure (13) that can adopt either a folded position or a deployed position.

机译：根据本发明，中心尖钉（ 7 ）的尖端（ 11 ）由可变形的结构（ 13 ）组成，该结构可以采取折叠位置或展开位置。 展开▼

著录项

公开/公告号US2003217552A1

专利类型

公开/公告日2003-11-27

原文格式PDF

申请/专利权人 CALABRO MAX;
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申请/专利号US20030436140

发明设计人 MAX CALABRO;
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申请日2003-05-13

分类号F02K1/06;

国家 US

入库时间 2022-08-21 23:15:41

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