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- W2318410190 abstract "HE future of human space exploration is being pursued by NASA through developing vehicle concepts that will enable short term missions from cislunar space. Possible missions include supporting a Near-Earth Asteroid capture, returning to the lunar surface and sending humans to Mars. A major focus was to keep the missions affordable by using existing spacecraft components. Another concern was to provide design flexibility that could accommodate various mission scenarios without developing new vehicles for each mission. A vital component of the mission architecture was the human habitat and life support system for a 75-day crew occupancy. One of the considerations for this habitat was to take the existing design of the Multi-Mission Space Exploration Vehicle (MMSEV) and develop multiple components around its core. Flexibility to operate various cislunar missions was added through a MMSEV derived Habitable Airlock (HAL) that provided crew accommodations and airlocks for the Orion MPCV (Multi-Purpose Crew Vehicle). To accomplish this, the HAL was developed into three and four node versions that could be combined and launched together in a single stack. Structural analysis was performed on various stack arrangements to investigate the structural and mass requirements to launch on the NASA’s new Space Launch System." @default.
- W2318410190 created "2016-06-24" @default.
- W2318410190 creator A5039632031 @default.
- W2318410190 date "2015-01-02" @default.
- W2318410190 modified "2023-09-25" @default.
- W2318410190 title "Structural Design of with Multi-Mission Space Exploration Vehicle (MMSEV)/Human Airlock (HAL) Concept Mission" @default.
- W2318410190 cites W2045528038 @default.
- W2318410190 doi "https://doi.org/10.2514/6.2015-1163" @default.
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