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Completed TRL 1 (started at 1, targeting 1)
Modular HSRV design includes a separable nose section with a unique propulsion system that nominally enables soft landing of the HSRV on the moon and Mars. #Nose sections are repurposable, providing crew recovery vehicle capabilities from surface or orbital nodes. In a contingency, the HSRV nose section separates along with the crew capsule to allow either ATO or abort-to-surface (ATS).#For Mars EDL ATS scenarios, the capsule separates from the nose section and employs a HIAD, supersonic parachutes, and retropropulsion to safely land.
Benefit to NASA human Moon and Mars exploration missions
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