Title:
FLYING OBJECT THRUSTER
Document Type and Number:
Japanese Patent JP2016044554
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To enable stable fuel injection by suppressing heat transfer to a propellant valve from a combustor in a flying object thruster.SOLUTION: The flying object thruster includes: an injector 11 for injecting fuel and an oxidant; the combustor 12 for combusting the fuel and oxidant injected from the injector 11; the propellant valve 13 for adjusting supply amounts of the fuel and oxidant; a capillary tube 14 for supplying the fuel and oxidant to the injector 11 from the propellant valve 13; and multiple struts 15 each having a hollow part 55 and connecting the propellant valve 13 and the injector 11.SELECTED DRAWING: Figure 1
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Inventors:
JOJIMA TAKAHIRO
Application Number:
JP2014166880A
Publication Date:
April 04, 2016
Filing Date:
August 19, 2014
Export Citation:
Assignee:
MITSUBISHI HEAVY IND LTD
International Classes:
F02K9/60
Attorney, Agent or Firm:
Hiroaki Sakai
Jun Takamura
Jun Takamura