Invention Grant
US08727283B2 Launch abort and orbital maneuver system 有权
发射中止和轨道机动系统

Launch abort and orbital maneuver system
Abstract:
A spacecraft includes a first engine configured to provide primary launch abort thrust and a second engine disposed radially from a center of gravity, the second engine configured to provide a secondary launch abort thrust, a primary orbital maneuvering thrust, and a primary control thrust.
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