The Boeing Company

Brian R Lindley

Jeffrey J Cronick

James K Wechsler

Jennifer L Green

Jon J Carpenter

Thomas Russell Smith

A returnable and reusable space vehicle including a main body separate from and releasably mounted to a booster rocket assembly. A crew compartment module is provided that is separate from and releasably mounted to the main body. A propellant system is operably coupled to the crew compartment module so as to propel the crew compartment module from the main body during an emergency procedure. An orientation control system is coupled to the propellant system such that the orientation control system maintains the crew compartment module in a predetermined attitude during the emergency procedure. A pair of aerodynamic lifting wings extend from the main body to provide aerodynamic lift the the main body to permit the main body to return from the orbit and land.

Crewed on-orbit, returnable, and reusable space vehicle

An orbit transfer vehicle for transporting cargo between a low Earth orbit and a higher Earth orbit having a body and an engine operably coupled to the body. A reaction control system is further provided and is operably coupled to the body. The reaction control system having a plurality of thrusters capable of maneuvering the orbit transfer vehicle. The orbit transfer vehicle further includes an energy absorbing panel operable to gather energy and an energy storage device operable to store the energy. Still further, a payload interface mechanism is provided having a payload container area and a payload retaining device. The payload retaining device is connectable to the cargo. Lastly, a controller for autonomously controlling the engine, the reaction control system, and the payload interface mechanism to control the orbit transfer vehicle so as to transport the cargo between a low Earth orbit to a higher Earth orbit.

Autonomous orbit transfer vehicle

A returnable and reusable space vehicle including a main body separate from and releasably mounted to a booster rocket assembly. A crew compartment module is provided that is separate from and releasably mounted to the main body. A propellant system is operably coupled to the crew compartment module so as to propel the crew compartment module from the main body during an emergency procedure. An orientation control system is coupled to the propellant system such that the orientation control system maintains the crew compartment module in a predetermined attitude during the emergency procedure. A pair of aerodynamic lifting wings extend from the main body to provide aerodynamic lift to the main body to permit the main body to return from the orbit and land.

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Corona Del Mar, CA, United States of America

Brian R Lindley