The Deep Space Systems Small Lunar Lander  (SLL) is designed to be launched into a Geosynchronous Transfer Orbit (GTO) as a secondary payload on any Launch Vehicle mission with ESPA* Grande capability.  From GTO the Lander completes all burns required to transfer to the Moon, enter lunar orbit, circularize into a low lunar orbit, and descend and land softly in a polar region.

*Evolved Expendable Launch Vehicle (EELV) Secondary Payload Adapter 

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