Vapor jetting device and spacecraft

Patent metadata

Field	Value
Publication number	US-9989012-B2
Application number	US-201514617341-A
Country	US
Kind code	B2
Filing date	Feb 9, 2015
Priority date	Aug 10, 2012
Publication date	Jun 5, 2018
Grant date	Jun 5, 2018

Abstract

Provided is a vapor jetting device including: a box-shaped casing; a propellant holding unit that is placed in the casing and forms a space for holding a propellant; a gas storing unit that is placed in the casing, forms a space that is divided from the propellant holding unit by a partition wall including a communication hole, and stores gas; a machine housing unit that is placed in the casing, forms a space that is divided from the propellant holding unit and the gas storing unit by partition walls, and houses machines; a nozzle that is connected to the casing and ejects the gas to an outside; a gas flow path that is formed in the casing and supplies the gas stored in the gas storing unit to the nozzle; and a heater that is placed in the casing and heats at least the gas storing unit.

First claim

The invention claimed is:

1. A spacecraft comprising:
a vapor jetting device that evaporates a propellant in the form of liquid to generate vapor and jets gas by means of a vapor pressure of the vapor to thereby obtain thrust to propel the spacecraft, the vapor jetting device comprising:
a cuboid-shaped casing;
a propellant holding unit that is placed in the cuboid-shaped casing and forms a first space for holding the propellant;
a gas storing unit that is placed in the cuboid-shaped casing, forms a second space that is divided from the propellant holding unit by a partition wall including a communication hole that provides fluid communication between the propellant holding unit and the gas storage unit, and stores the gas;
a machine housing unit that is placed in the cuboid-shaped casing, forms a third space that is divided from the propellant holding unit and the gas storing unit by partition walls, and houses machines;
a nozzle that is connected to the cuboid-shaped casing and ejects the gas to an outside;
a gas flow path that is formed in the cuboid-shaped casing and supplies the gas stored in the gas storing unit to the nozzle; and
a heater that is placed in the cuboid-shaped casing and heats at least the gas storing unit wherein the propellant holding unit comprises:
a fill and drain port for pouring or discharging the propellant, wherein the propellant holding unit is between the fill and drain port and the gas storing unit; and
a plurality of propellant holding plates that are placed about the fill and drain port and generate surface tension on the propellant to thereby hold the propellant, wherein the fill and drain port is configured to discharge the propellant between the plurality of propellant holding plates.

2. The spacecraft according to claim 1 , wherein the gas storing unit includes: a gas outlet for discharging the gas; and a heat spreader placed between the gas outlet and the communication hole.

3. The spacecraft according to claim 2 , wherein a gas supply tube, that connects the gas outlet to the gas flow path, is arranged in the machine housing unit, and
a valve that controls ejection of the gas is provided to the gas supply tube.

4. The spacecraft according to claim 2 , wherein the heater is placed at a position adjacent to the heat spreader.

5. The spacecraft according to claim 1 , wherein a filter that suppresses the propellant in the form of liquid from entering the gas storing unit is placed in the communication hole.

6. The spacecraft according to claim 1 , wherein the heater is controlled such that a temperature of the gas storing unit becomes higher than a temperature of the propellant holding unit.

7. The spacecraft according to claim 1 , wherein the cuboid-shaped casing is stackable on an additional module having the same shape.

8. The spacecraft according to claim 7 , wherein the additional module is at least one of: an additional tank that stores the propellant; a battery module on which a battery is mounted; a monitoring module on which a monitoring machine or a measuring machine is mounted; and a control module that controls machines mounted on the vapor jetting device or the additional module.

Assignees

• Ihi Corp
• Ihi Aerospace Co Ltd

Inventors

• Izumiyama Taku
• Mori Hatsuo
• Hashimoto Kozue
• Nagao Toru

Classifications

• F02K9/94

  Re-ignitable or restartable rocket- engine plants; Intermittently operated rocket-engine plants · CPC title

• B64G1/40 Primary

  Arrangements or adaptations of propulsion systems · CPC title

• F02K9/44

  Feeding propellants · CPC title

• B64G1/26

  using jets · CPC title

• F02K7/02 Primary

  the jet being intermittent, i.e. pulse-jet · CPC title