| 发明名称 |
COMBINED LAUNCH AND MISSION VEHICLES |
| 摘要 |
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. |
| 申请公布号 |
US2015353197(A1) |
申请公布日期 |
2015.12.10 |
| 申请号 |
US201514685054 |
申请日期 |
2015.04.13 |
| 申请人 |
Sikorsky Aircraft Corporation |
发明人 |
Alber Mark R. |
| 分类号 |
B64D5/00;B64C29/00 |
主分类号 |
B64D5/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft, comprising:
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 being umbilically coupled to the mission vehicle during the VTO operations and releasable from the mission vehicle thereafter. |
| 地址 |
Stratford CT US |
