Skyrora XL is a three-stage small-launch vehicle, intended for placing payloads into Sun-Synchronous Orbit (SSO) between 500-1000 km in altitude, as well as Polar Orbit (PO) between 200-1000 km.

One of the key advantages of the Skyrora XL is the combined manufacturing process of all main systems, its assembly and integration. It is designed to reduce the time and cost in the manufacturing/assembly process, whilst also improving the reliability of the whole launch vehicle. 

In order to meet the customer’s payload requirements, we use an encapsulated payload module, which is assembled as a separate system away from the remainder of the launch vehicle, providing far more flexibility for launch and for customers. 

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