MULTIPLE-USE ROCKET ENGINES AND ASSOCIATED SYSTEMS AND METHODS
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United States of America Patent
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Issued Date -
Dec 30, 2010
app pub date -
Feb 12, 2010
filing date -
Feb 13, 2009
priority date (Note) -
Abandoned
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Abstract
Multiple-use rocket engines and associated systems and methods are disclosed. A method in accordance with a particular embodiment includes launching a two-stage vehicle have a first stage and a second stage carried by the first stage. The first stage can be powered with a first rocket engine having first rocket engine components, including a first combustion chamber, arranged in a first component configuration. The method can further include separating the second stage from the first stage, and powering the second stage with a second rocket engine having second engine components arranged in a second component configuration. The second rocket engine components can include a second combustion chamber that is interchangeable with the first combustion chamber. In further particular embodiments, recovered engine components from the first stage may be used to power the second stage of the same or a different two-stage vehicle.
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