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US 2026/0152295 A1Published application
Propellant supply system
AssigneeJapan Aerospace Exploration Agency
InventorsMitsuru SHIMAGAKI, Toshiya KIMURA, Satoshi TAKADA
Life of this patent
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Abstract
A propellant supply system (100) for supplying fuel (F) and oxidizer (O) to a propellant supply target (R) includes: an axial gap motor (10) having a rotating shaft, a fuel pump (30) provided at one end of the rotating shaft, and an oxidizer pump (40) provided at the other end of the rotating shaft.
Claims7
A propellant supply system for supplying fuel and oxidizer to a propellant supply target, comprising:
- an axial gap motor having a rotating shaft;
- a fuel pump provided at one end of the rotating shaft;
- and
- an oxidizer pump provided at the other end of the rotating shaft.
1 more element
Dependencies are inferred from the claim text.