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Title:
SOLID ROCKET
Document Type and Number:
Japanese Patent JP2003118700
Kind Code:
A
Abstract:

To solve a problem of massive expenses due to developing of a core rocket or an exclusive booster rocket in response to an operation purpose.

The solid rocket R is provided with a main rocket 1 loaded with solid propellant and a sub rocket 2 loaded with solid propellant and smaller than the main rocket 1. A plurality of the sub rockets 2 are selectively attached to the main rocket 1 in response to the operation purpose. A thrust level or a thrust pattern responding to operation is generated and a development cost is markedly reduced.


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Inventors:
MAKINO TAKASHI
YAMAMOTO YOICHI
YAGI KAZUHIRO
Application Number:
JP2001317003A
Publication Date:
April 23, 2003
Filing Date:
October 15, 2001
Export Citation:
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Assignee:
IHI AEROSPACE CO LTD
International Classes:
B64G1/00; (IPC1-7): B64G1/00
Attorney, Agent or Firm:
Matoba



 
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