By comparison, the Saturn V had a Payload to LEO (Low Earth Orbit) of 310,000 lbs, and a Payload to TLI (Trans Lunar Injection, whatever that is) of 107,100 lbs.
But it was not reusable.
Trans Lunar Injection is the point where the vehicle leaves earth orbit and begins the Trans Lunar Coast toward the moon. You then have Lunar Orbit Injection, Lunar Orbit, Trans Earth injection, Trans Earth Coast, Earth Orbit Injection, Earth Orbit again and then Re-entry. All require rocket burns.
Yes, I used to work there. Just celebrated the Christmas ‘68 Apollo 8 mission.