Title:
スペースクラフト（ｓｐａｃｅｃｒａｆｔ）後部胴体装置
Document Type and Number:
Japanese Patent JP5677092
Kind Code:
B2
Abstract:
An afterbody device for a spacecraft fitted with at least one rocket engine at the rear of the craft includes at least one movable cover element designed to take a first position, masking and reducing the vehicle's rear drag, where it prolongs the vehicle's fuselage around at least one part of a rocket engine nozzle of the vehicle and extends beyond the rear of the vehicle's fuselage, and to take a second position fully deployed, increasing the vehicle's aerodynamic drag.
Inventors:
プランポリーニ、マルコ
Application Number:
JP2010535344A
Publication Date:
February 25, 2015
Filing Date:
November 21, 2008
Export Citation:
Assignee:
アストリウム・エス・エー・エス
International Classes:
B64G1/14; B64C9/32; B64C15/00; B64G1/40; F02K9/84
Attorney, Agent or Firm:
Hill 有