Abstract: A reusable spacecraft system having two substantially identically reusable return flight space vehicles, one of which is preferably a booster and the other an orbiter, each of which have identical flight control and propulsion systems and have identical but selectably installable components, such as thermal protection disposed on the orbiter but not on the booster. Each vehicle further includes identical payload bays for receiving mission specific payloads, that may be for example, a propellant tankage payload for the booster and a manned mission payload for the orbiter. The use of identical booster and orbiter vehicles reduces costs of development, production and reusable missions.