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Thruster tank with on-off gas flow control system, thruster and spacecraft incorporating such a control system
Thruster tank with on-off gas flow control system, thruster and spacecraft incorporating such a control system
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机译：具有开关气流控制系统的推进器箱，推进器和装有该控制系统的航天器
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摘要
The invention relates to a reservoir (1) for a solid or liquid propellant (2) for a propellant, the reservoir (1) comprising means for forming a gas (9) in the reservoir, the reservoir (1) having an opening ( 4) of surface S to extract from the reservoir (1) a flow (20) of the propellant gas. According to the invention, the reservoir (1) comprises an on-off control system for the flow of the propellant gas comprising a grid (6) disposed facing the opening (4) of the reservoir (1), a first system thermal regulation system (11, 21) adapted to heat the gas (9) in the tank and a second thermal regulation system (12, 22) adapted to heat the grid (6), the grid (6) having surface orifices total greater than the surface S of the opening of the tank (1). Figure for the abstract: Fig. 1
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