Title:
触媒スラスタ
Document Type and Number:
Japanese Patent JP7406631
Kind Code:
B2
Abstract:
A monopropellant thruster according to an exemplary aspect of the present disclosure includes, among other things, a first part having a catalyst bed, a thrust chamber, and a nozzle. The first part is integrally formed via a single additive manufacturing process. The thruster further includes a second part, which is a closeout. A method is also disclosed.
Inventors:
Yarnot, Vincent Shi.
Stanley, Stephen
urban, galette
Jakbek, Matthew Tee.
Argust, Ronald El.
Stanley, Stephen
urban, galette
Jakbek, Matthew Tee.
Argust, Ronald El.
Application Number:
JP2022528215A
Publication Date:
December 27, 2023
Filing Date:
November 22, 2019
Export Citation:
Assignee:
Aerojet Rocketdyne Incorporated
International Classes:
F02K9/62; B22F10/25; B33Y80/00; F02K9/52; F02K9/97
Foreign References:
| KR101969901B1 | ||||
| US20170037814 | ||||
| US4352782 |
Attorney, Agent or Firm:
Hiromichi Kobayashi
Kiyoshi Tomioka
Kiyoshi Tomioka
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