|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/245; 60/251; 60/253; 60/2701|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 1|
A solid fuel propulsion system for a ran jet rocket having a combustion chamber (B) surrounded by a tubular casing (2) and a gas generator (G) disposed upstream from the combustion chamber (B) and surrounded by a tubular casing (1) for generation of a combustible gas from a solid fuel, disposed between the gas generator (G) and the combustion chamber (B) is a gas-stream regulator unit (R) for regulation of the flow of the combustible gas from the gas generator (G) to the combustion chamber (B). The propulsion system has a middle section (4) in which the ...
1. A solid fuel propulsion system for a ram jet rocket comprising:a combustion chamber having an outer tubular casing, a gas generator disposed downstream of said combustion chamber for generating a combustible gas from a solid fuel in said gas generator, said gas generator having an outer tubular casing, a gas flow regulator disposed between said combustion chamber and said gas generator for regulating a stream of combustible gas from said gas generator to said combustion chamber, a middle section secured between said gas generator and said combustion c...