Diana II Vision
Our vision is to enable a sustainable presence on the lunar south pole to bring humanity one step closer to exploring deeper into our solar sysytem.
Mission
Site Selection Criteria
Establish a base with a minimal footprint to extract and process lunar ice found in permanently shadowed regions.
Peak Near Shackleton
Faustin Rim A
Connecting Ridge
Illumination
Requirements • architecture and systems must support a crew of 4 for up to 14 days. • Each surface element shall not exceed a dry mass of 6,000 kg. • Surface elements must consider future base expansion where crew size and duration will increase.
Slope
POIs
Design Drivers • Minimize EVAs. • Consider environmental factors of the lunar south pole. • Provide redundant power sources for reliability and safety in the concept of operations. • Enable autonomous ISRU (ice extraction). • Offloading and manifesting assets from one Human Landing System (HLS Starship) per mission. • Utilization of modular mobility platform for all surface assets.
Habitat #1 + MMP #3 Sleeping Quarters Hygeine Facilitieis Water Storage Solar Storm Shelter
Pressurized Rover #1 + MMP #2
D i a n a
I
MMP #3 with Robotic Arm Attachment and Undeployed Nuclear Reactor
Habitat #2 + MMP #4 Medical Galley Labratory Recreation
Habitat #3 + MMP #5 Suitlock EVA Maintnance Area Dusty Storage
D i a n a
Pressurized Rover #2 + MMP #6
II