Combined launch and mission vehicles
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United States of America Patent
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Sep 12, 2017
Issued Date -
N/A
app pub date -
Apr 13, 2015
filing date -
Jun 10, 2014
priority date (Note) -
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Abstract
An aircraft is provided and includes a mission vehicle configured to follow vertical take-off and landing (VTOL) operations and to execute forward flight, hover/loiter and landing operations and a launch vehicle configured to drive the mission vehicle through at least vertical take-off (VTO) operations. The launch vehicle is umbilically coupled to the mission vehicle during the VTO operations and releasable from the mission vehicle thereafter.
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