公开(公告)号：US20150144738A1

公开(公告)日：2015-05-28

申请号：US14405947

申请日：2013-06-03

Applicant: SNECMA

Inventor： Nicolas Soulier ,  Maxime Vicentini ,  Jean-Marie Conrardy

IPC: B64G1/24 ,  B64G1/40

CPC classification number: B64G1/242 ,  B64G1/26 ,  B64G1/40 ,  B64G1/401 ,  B64G1/402 ,  F02K9/766

Abstract: A spacecraft including at least one main propellant tank, a main engine fed with propellant by the main tank, and a de-orbiting device. The de-orbiting device includes a detonation engine fed with propellant by the main tank.

Abstract translation: 包括至少一个主推进剂罐，由主油箱供给推进剂的主发动机和离轨装置的航天器。 离轨装置包括由主油箱供给推进剂的爆震发动机。

公开(公告)号：US09487310B2

公开(公告)日：2016-11-08

申请号：US14405947

申请日：2013-06-03

Applicant: SNECMA

Inventor： Nicolas Soulier ,  Maxime Vicentini ,  Jean-Marie Conrardy

IPC: B64G1/26 ,  B64G1/40 ,  F02K9/76 ,  B64G1/24

CPC classification number: B64G1/242 ,  B64G1/26 ,  B64G1/40 ,  B64G1/401 ,  B64G1/402 ,  F02K9/766

Abstract: A spacecraft including at least one main propellant tank, a main engine fed with propellant by the main tank, and a de-orbiting device. The de-orbiting device includes a detonation engine fed with propellant by the main tank.

Abstract translation: 包括至少一个主推进剂罐，由主油箱供给推进剂的主发动机和离轨装置的航天器。 离轨装置包括由主油箱供给推进剂的爆震发动机。