Vented launch vehicle adaptor for a manned spacecraft with pusher launch abort system
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United States of America Patent
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May 12, 2020
Grant Date -
Aug 10, 2017
app pub date -
Apr 28, 2017
filing date -
Jul 20, 2011
priority date (Note) -
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Abstract
A system, method, and apparatus for a vented launch vehicle adaptor (LVA) for a manned spacecraft with a “pusher” launch abort system are disclosed. The disclosed LVA provides a structural interface between a commercial crew vehicle (CCV) crew module/service module (CM/SM) spacecraft and an expendable launch vehicle. The LVA provides structural attachment of the module to the launch vehicle. It also provides a means to control the exhaust plume from a pusher-type launch abort system that is integrated into the module. In case of an on-pad or ascent abort, which requires the module to jettison away from the launch vehicle, the launch abort system exhaust plume must be safely directed away from critical and dangerous portions of the launch vehicle in order to achieve a safe and successful jettison.
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