Hideshi Kagawa Go Fujii Kenichi Kajiwara Daisuke Kuroda Takuya Suzuki Yoko Yamabe-Mitarai Hideyuki Murakami Yoshinori Ono
European Space Agency, (Special Publication) ESA SP 691 SP 2012年
Haynes25 (L-605) is a common heat resistant alloy used in mono-propellant structures and screen materials for catalyst beds. The lifetime requirements for thrusters have expanded dramatically after studies conducted in the 1970s on mono-propellant...
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011 2011年
Most mono-propellant thruster technologies were developed in the 1960s and the basic principles and fundamental structures, such as the catalyst and propellant, have remained in use without major technical innovation. Conversely, much remains to b...
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011 2011年
Monopropellant Hydrazine Thrusters are widely used in many satellites and explorers propulsion systems and launch vehicle RCSs due to their simple and low cost features. The first generation Japanese 1N thruster design is based on the US TRW 1970s...
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2009年
Haynes25 (L-605) is a common heat resistant alloy used in mono-propellant structures and in screen materials for catalyst beds. The lifetime requirements for thrusters have expanded dramatically after studies conducted in the 1970s on mono-propell...
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2009年
The Low specific-speed (Ns) pump is well known for its low pump efficiency, due to large flow-pass chafe and volute matching loss. Last year, we reported a new low Ns high-pressure-pump design. In the report we made two types of impeller and teste...
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