| 摘要 |
A remote controlled aircraft may include a deployable main parachute, deployable paratroopers stored in the coils of helical spring actuator and moved into deployment position by rotation of the actuator. The actuator may be operated within a storage compartment configured to fit the actuator and to maintain alignment of the paratroopers before deployment. The remote control may include individual engine boost buttons and selectable, preprogrammed engine speeds. A secondary remote controlled aircraft may also be mounted for deployment on the main aircraft. Various configurations and combinations of elements and features are disclosed and may be claimed.
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