Title:
推進装置、飛行体及び推進方法
Document Type and Number:
Japanese Patent JP7451209
Kind Code:
B2
Abstract:
A propulsion apparatus is provided with a gas generator and a plurality of thrusters. The gas generator generates combustion gas when a flying body satisfies an emergency condition. Herein, the plurality of thrusters output the combustion gas downward. In addition, when viewed from a direction of travel of the flying body, the plurality of thrusters may overlap the gas generator. Furthermore, the plurality of thrusters may control an attitude of the flying body. In addition, the plurality of thrusters may reduce outputs of the combustion gas to a first output based on a landing of at least a part of the flying body.
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Inventors:
Masayuki Eguchi
Toshiharu Fujita
Yukihiro Okumura
Toshiharu Fujita
Yukihiro Okumura
Application Number:
JP2020022075A
Publication Date:
March 18, 2024
Filing Date:
February 13, 2020
Export Citation:
Assignee:
MITSUBISHI HEAVY INDUSTRIES,LTD.
International Classes:
B64D25/00; B60F5/02; F02K1/78
Domestic Patent References:
| JP2018111474A | ||||
| JP2018537361A | ||||
| JP6425323B1 | ||||
| JP2001322600A | ||||
| JP8192796A |
Foreign References:
| US20030042367 |
Attorney, Agent or Firm:
Takaharu Fujita
Takaori Mitoma
Miki Kawakami
Daisuke Nagata
Yoshimasa Kano
Keisaku Nakao
Takaori Mitoma
Miki Kawakami
Daisuke Nagata
Yoshimasa Kano
Keisaku Nakao