Abstract:
A vertical take-off and landing (VTOL) vehicle includes a first thruster, a first duct, a second thruster, a second duct, an engine pod, and a transport unit. The first duct is configured to direct airflow generated by the first thruster. The second duct is configured to direct airflow generated by the second thruster. The engine pod is formed between the first duct and the second duct. The transport unit is formed between the first duct and the second duct, and is configured to transport a person or another payload. The transport unit is alternatively a person transport or a surveillance package pod.