发明名称 SOLID PROPELLANT FOR END BURNING AND METHOD FOR MANUFACTURING THE SAME
摘要 PROBLEM TO BE SOLVED: To provide a soil propellant for end surface combustion capable of keeping generation quantity of combustion gas and thrust constant without fluctuation. SOLUTION: This solid propellant is manufactured by applying an adhesive layer 3 for improving adhesion force of an insulation and propellant on an inside of the insulation 1 formed in a cylindrical shape and then filling slurry propellant 2 inside, and heating and hardening the same. When a liner layer 4 is applied on an inside of the adhesive layer 3, slurry propellant 2 is filled inside the liner layer 4 after hardening reaction of the applied liner layer 4 completes, and the propellant 2 is heated and hardened. COPYRIGHT: (C)2007,JPO&INPIT
申请公布号 JP2007138796(A) 申请公布日期 2007.06.07
申请号 JP20050332609 申请日期 2005.11.17
申请人 IHI AEROSPACE CO LTD;NOF CORP 发明人 MATSUURA ARATA;NAGASE SAKAE;KOBAYASHI YASUSHI
分类号 F02K9/10 主分类号 F02K9/10
代理机构 代理人
主权项
地址