Title:
GAS RESERVOIR FOR AEROSPACE VEHICLE, AND AEROSPACE VEHICLE
Document Type and Number:
WIPO Patent Application WO/2015/029146
Kind Code:
A1
Abstract:
A gas reservoir (10) for a rocket is provided to a rocket provided with a frame configured using a hollow cylindrical strength member. The gas reservoir (10) is provided with a gas-reservoir structure (20) which is capable of accumulating a working gas inside the strength member (13). The gas-reservoir structure (20) is provided with: a pair of tube plates (21, 22) which are provided inside the strength member (13), and which face each other; and a filling fitting (23) and a discharge fitting (23) which are provided to one of the tube plates (21), and which have, connected thereto, piping for causing the working gas to circulate in and out of the strength member (13) partitioned by the pair of tube plates (21, 22).
Inventors:
KUSABA NAOKI (JP)
SATO AKIHIRO (JP)
SATO AKIHIRO (JP)
Application Number:
PCT/JP2013/072921
Publication Date:
March 05, 2015
Filing Date:
August 27, 2013
Export Citation:
Assignee:
MITSUBISHI HEAVY IND LTD (JP)
International Classes:
B64G1/40
Foreign References:
| JPH02500100A | 1990-01-18 | |||
| US20100012788A1 | 2010-01-21 | |||
| JP2008189304A | 2008-08-21 | |||
| JP2000220795A | 2000-08-08 | |||
| JPH0381551A | 1991-04-05 |
Attorney, Agent or Firm:
SAKAI, Hiroaki et al. (JP)
Hiroaki Sakai (JP)
Hiroaki Sakai (JP)
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