Launch and capture systems for vertical take-off and landing (VTOL) vehicles
A launch and capture system for capturing a vertical take-off and landing (VTOL) vehicle having a thruster and a duct configured to direct airflow generated by the thruster includes a capture plate and an extension. The capture plate is configured to alter the airflow and generate a force attracting the duct to the capture plate. The extension is coupled to the capture plate, and is configured to at least facilitate holding the VTOL vehicle against the capture plate.
1. A launch and capture system for capturing a vertical take-off and landing (VTOL) vehicle comprising a thruster and a duct configured to direct airflow generated by the thruster, the launch and capture system comprising:
a capture plate configured to alter the airflow and generate a force attracting the duct to the capture plate; and
an extension coupled to the capture plate and configured to at least facilitate holding the VTOL vehicle against the capture plate.
2. The launch and capture system of claim 1 , further comprising: a mast coupled to the capture plate.
3. The launch and capture system of claim 2 , further comprising: a lift system coupled to the mast and configured to lift the mast.
4. The launch and capture system of claim 1 , wherein the capture plate comprises a plurality of ports movable between an open position and a closed position.
5. The launch and capture system of 4 , wherein the plurality of ports are configured to increase the force attracting the duct to the capture plate when at least one of the plurality of ports is moved from the open position to the closed position.
6. The launch and capture system of claim 1 , further comprising:
a rod coupled to the capture plate and configured to selectively at least facilitate separation of the VTOL vehicle from the capture plate.
7. The launch and capture system of claim 1 , further comprising:
a mounting device configured to mount the launch and capture system to a recovery vehicle; and
a shock absorber coupled between the mounting device and the capture plate and configured to absorb shock from the recovery vehicle.
8. The launch and capture system of claim 1 , further comprising:
a servo system configured to orient the capture plate.
9. A launch and capture system for capturing a vertical take-off and landing (VTOL) vehicle comprising a thruster and a duct configured to direct airflow generated by the thruster, the launch and capture system comprising:
a capture plate configured to alter the airflow and generate a force attracting the duct to the capture plate, the capture plate comprising a plurality of ports movable between an open position and a closed position; and
a mast coupled to the capture plate.
10. The launch and capture system of claim 9 , further comprising:
an extension configured to at least facilitate holding the VTOL vehicle against the capture plate.
11. The launch and capture system of claim 9 , further comprising:
a rod coupled to the capture plate and configured to selectively at least facilitate separation of the VTOL vehicle from the capture plate.
12. The launch and capture system of claim 9 , further comprising:
a lift system coupled to the mast and configured to lift the mast.
13. The launch and capture system of claim 9 , further comprising:
a mounting device configured to mount the launch and capture system to a recovery vehicle; and
a shock absorber coupled between the mounting device and the capture plate and configured to absorb shock from the recovery vehicle.
14. The launch and capture system of claim 9 , further comprising:
a servo system configured to orient the capture plate.
15. The launch and capture system of claim 9 , further comprising the vertical take-off and landing (VTOL) vehicle comprising the thruster and the duct configured to direct airflow generated by the thruster.
16. The launch and capture system of 9 , wherein the plurality of ports are configured to increase the force attracting the duct to the capture plate when at least one of the plurality of ports is moved from the open position to the closed position.
17. A method comprising:
capturing, using a capture plate, a vertical take-off and landing (VTOL) vehicle comprising a thruster and a duct configured to direct airflow generated by the thruster, wherein the capture plate is configured to alter the airflow and generate a force attracting the duct to the capture plate; and
engaging with the VTOL an extension coupled to the capture plate to assist holding the VTOL against the capture plate.
18. The method of claim 17 , wherein the capture plate comprises a plurality of ports movable between an open position and a closed position, the method further comprising: moving at least one of the plurality of ports between the open position and the closed position to increase the force attracting the duct to the capture plate.
19. The method of claim 17 , wherein the capture plate comprises a plurality of ports movable between an open position and a closed position, the method further comprising moving at least one of the plurality of ports between the closed position and the open position to decrease the force attracting the duct to the capture plate.