Flight systems

1. A thrust system, comprising:

a thrust engine oriented in a substantially vertical direction to provide vertical take-off and landing capability and configured to provide a thrust output, comprising one or more exhausted fluid outputs, substantially along a first axis;

a deflector assembly movably coupled to the thrust engine,

wherein the deflector assembly includes a pair of deflecting guides, each deflecting guide of said pair of deflecting guides being independently movable one from another to selectively deflect a portion of one of said one or more exhausted fluid outputs to divert said one of said one or more exhausted fluid outputs into at least two thrust vectors angled with respect to the first axis, and

wherein the deflecting guides are displaceable toward and away from each other between a closed configuration in which the deflecting guides are juxtaposed against one another and are within a path of the exhausted fluid output, and an open configuration in which the deflecting guides are apart and out of the path of the exhausted fluid output.

2. The thrust system according to claim 1 , wherein at least two thrust vectors all have substantially the same magnitude.

3. The thrust system according to claim 1 , wherein each thrust vector is angled between 45 degrees and 90 degrees with respect to the first axis.

4. The thrust system according to claim 1 , wherein each thrust vector has substantially the same angle with respect to the first axis.

5. The thrust system according to claim 1 , wherein the deflecting guides each define a substantially curvilinear surface that deflects said one of said one or more exhausted fluid outputs.

6. The thrust system according to claim 1 , wherein the deflecting guides each define a surface having a substantially semicircular cross-section that deflects said one of said one or more exhausted fluid outputs.

7. The thrust system according to claim 1 , wherein the deflecting guides are pivotable with respect to the thrust engine.

8. The thrust system according to claim 1 , wherein the thrust engine is one of a turbojet engine, a turbofan engine, and a turboprop engine.

9. The thrust system according to claim 1 , wherein, in the closed configuration, the deflecting guides reduce a vertical component of the thrust output without reversing its direction.

10. The thrust system according to claim 1 , further comprising at least two actuators coupled to the respective deflecting guides to controllably adjust a position of the respective deflecting guides with respect to the thrust engine.

11. The thrust system according to claim 10 , further comprising a controller in communication with the at least two actuators, wherein the controller is configured to operate the at least two actuators in response to one or more signals from at least one of an operator and a sensor.

12. The thrust system according to claim 1 , wherein the respective deflecting guides are each substantially planar and oriented in a plane substantially perpendicular to the first axis.

13. The thrust system according to claim 12 , wherein the deflecting guides are movable towards and away from one another within the plane.

14. The thrust system according to claim 1 , wherein the deflecting guides are pivotable about a second axis substantially perpendicular to the first axis.

15. The thrust system according to claim 14 , wherein the second axis is located above the thrust output of the thrust engine.

16. A propulsion device, comprising:

a platform configured to support a passenger thereon; and

a thrust system according to claim 1 coupled to the platform.