US Patent 8727283 Launch abort and orbital maneuver system
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Patent 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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Patent Inventor Names
Alfred Little0
Dennis E. Morris0
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US Patent 08727283 Launch abort and orbital maneuver system US Patent 8727283 Launch abort and orbital maneuver system
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Patent Number
087272830
Patent Number
87272830
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Patent Jurisdiction
Patent Number
087272830
Date of Patent
May 20, 2014
0Patent Application Number
131548730
Date Filed
June 7, 2011
0Official Website
Patent Primary Examiner
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US Patent 08727283 Launch abort and orbital maneuver system
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Is a
Patent jurisdiction
Patent number
08727283
Date of patent
May 20, 2014
Patent application number
13154873
Date Filed
June 7, 2011
Patent primary examiner
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