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Advanced Spacecraft Designs in Support of Human Missions to Earth's NeighborhoodNASA's strategic planning for technology investment draws on engineering studies of potential future missions. A number of hypothetical mission architectures have been studied. A recent study completed by The NASA/JSC Advanced Design Team addresses one such possible architecture strategy for missions to the moon. This conceptual study presents an overview of each of the spacecraft elements that would enable such missions. These elements include an orbiting lunar outpost at lunar L1 called the Gateway, a lunar transfer vehicle (LTV) which ferries a crew of four from the ISS to the Gateway, a lunar lander which ferries the crew from the Gateway to the lunar surface, and a one-way lunar habitat lander capable of supporting the crew for 30 days. Other supporting elements of this architecture discussed below include the LTV kickstage, a solar-electric propulsion (SEP) stage, and a logistics lander capable of re-supplying the 30-day habitat lander and bringing other payloads totaling 10.3 mt in support of surface mission activities. Launch vehicle infrastructure to low-earth orbit includes the Space Shuttle, which brings up the LTV and crew, and the Delta-IV Heavy expendable launch vehicle which launches the landers, kickstage, and SEP.
Document ID
20110000669
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Fletcher, David
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 25, 2013
Publication Date
February 3, 2002
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-7080
Meeting Information
Meeting: Space Technology and Applications International Forum (STAIF-2000)
Location: Albuquerque, NM
Country: United States
Start Date: February 3, 2002
End Date: February 7, 2002
Sponsors: Institute for Space and Nuclear Power Studies
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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