Launch pad system
A launch pad system includes a fuel vent port provided in a launch vehicle, a launch pad fuel tank provided outside the launch vehicle to store fuel, a fuel recovery line connecting the fuel vent port and the launch pad fuel tank such that the fuel is transferred therethrough, and a fuel transfer unit provided on the fuel recovery line to transfer the fuel, wherein the fuel may be recovered from the launch vehicle to the launch pad fuel tank.
1 . A launch pad system, comprising:
a fuel vent port provided in a launch vehicle;
a launch pad fuel tank provided outside the launch vehicle to store fuel;
a fuel recovery line connecting the fuel vent port and the launch pad fuel tank such that the fuel is transferred therethrough;
a fuel transfer unit provided on the fuel recovery line to transfer the fuel;
a fuel vent valve provided on the fuel recovery line;
an oxidizer vent port provided in the launch vehicle;
a launch pad oxidizer tank provided outside the launch vehicle to store an oxidizer;
an oxidizer recovery line connecting the oxidizer vent port and the launch pad oxidizer tank such that the oxidizer is transferred therethrough; and
an oxidizer vent valve provided on the oxidizer recovery line, wherein the fuel is recovered from the launch vehicle to the launch pad fuel tank;
wherein the oxidizer vent port is a separate and distinct element from the fuel vent port,
wherein a portion of the fuel is discharged to the outside through the fuel vent valve,
wherein the fuel vent valve is provided on a branched line between the fuel vent port and the fuel transfer unit on the fuel recovery line, and
wherein a portion of the oxidizer is discharged to the outside through the oxidizer vent valve.
2 . The launch pad system of claim 1 , further comprising:
a freezing unit provided on the fuel recovery line to cool the fuel,
wherein the fuel is liquefied through the freezing unit and introduced into the launch pad fuel tank.
3 . The launch pad system of claim 1 , further comprising:
a fuel inlet port provided in the launch vehicle and connected to the launch pad fuel tank; and
a fuel supply line connecting the launch pad fuel tank and the fuel inlet port to supply the fuel to the launch vehicle,
wherein the fuel stored in the launch pad fuel tank is supplied to the launch vehicle through the fuel supply line and the fuel inlet port.
4 . The launch pad system of claim 1 , wherein
the launch vehicle comprises a first-stage launch vehicle and a second-stage launch vehicle, and
the fuel recovery line comprises:
a first fuel recovery line connected to the first-stage launch vehicle; and
a second fuel recovery line connected to the second-stage launch vehicle.
5 . The launch pad system of claim 1 , further comprising:
an oxidizer transfer unit provided on the oxidizer recovery line to transfer the oxidizer,
wherein the oxidizer is recovered from the launch vehicle to the launch pad oxidizer tank via the oxidizer recovery line.
6 . The launch pad system of claim 1 , further comprising:
a fuel cell connected to the launch pad fuel tank and the launch pad oxidizer tank,
wherein the fuel is hydrogen,
the oxidizer is oxygen, and
the fuel cell receives the hydrogen from the launch pad fuel tank and receives oxygen from the launch pad oxidizer tank to generate electricity.
7 . The launch pad system of claim 1 , further comprising:
an engine cooling port provided in the launch vehicle;
an engine cooling line connecting the engine cooling port and the launch pad fuel tank such that the fuel is transferred therethrough;
an engine cooling transfer unit provided on the engine cooling line to transfer the fuel; and
an engine cooling freezing unit provided on the engine cooling line to cool the fuel,
wherein the engine cooling line controls an output of the engine cooling transfer unit and an output of the engine cooling freezing unit through interoperation with a temperature sensor and a pressure sensor in an engine.