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.
Combined launch and mission vehicles
2017-09-12
Patent
Electronic Resource
English
Minotaur-Family Launch Vehicles Responsive Launch Demonstration for the TacSat-2 Mission AIAA Paper
British Library Conference Proceedings | 2007
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