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US 11,236,703 B2Granted
Dual stage catalytic thruster
AssigneeAerojet Rocketdyne, Inc.
InventorsMatthew Dawson, Gerald Brewster
Life of this patent
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Abstract
A catalytic thruster includes a reaction chamber that extends between first and second opposed chamber ends. The first chamber end includes a thermal standoff cup. There is a catalyst bed in the reaction chamber, and a feed tube extends into the reaction chamber through the thermal standoff cup.
Claims12
A catalytic thruster comprising:
- a reaction chamber that extends between a first chamber end and a second chamber end, the first chamber end including a thermal standoff cup;
- a catalyst bed in the reaction chamber, the thermal standoff cup bounding the catalyst bed;
- a feed tube that extends into the reaction chamber through the thermal standoff cup, the feed tube includes a tube end that has at least one injection port that opens into the reaction chamber;
- and
- a sacrificial flow restrictor that partially blocks the at least one injection port, wherein the sacrificial flow restrictor is formed of a material that degrades and sheds from the at least one injection port upon operation of the catalytic thruster,
- the feed tube extending a distance D1 into the reaction chamber, the distance D1 being defined from an inside surface of a narrow bottom of the thermal standoff cup where the feed tube enters to a tip of the feed tube in the reaction chamber, the reaction chamber is disposed about a central axis and has a radial dimension D2 relative to the central axis, and a penetration ratio of the distance D1 to the radial dimension D2 is greater than or equal to 1:1.
3 more elements
Dependencies are inferred from the claim text.