Lunar Lander Conceptual Design
Lunar Lander Conceptual Design
- New search for: J. A. Lee
- New search for: J. Carini
- New search for: A. Choi
- New search for: R. Dillman
- New search for: S. J. Griffin
- New search for: J. A. Lee
- New search for: J. Carini
- New search for: A. Choi
- New search for: R. Dillman
- New search for: S. J. Griffin
A conceptual design is presented of a Lunar Lander, which can be the primary vehicle to transport the equipment necessary to establish a surface lunar base, the crew that will man the base, and the raw materials which the Lunar Station will process. A Lunar Lander will be needed to operate in the regime between the lunar surface and low lunar orbit (LLO), up to 200 km. This lander is intended for the establishment and operation of a manned surface base on the moon and for the support of the Lunar Space Station. The lander will be able to fulfill the requirements of 3 basic missions: A mission dedicated to delivering maximum payload for setting up the initial lunar base; Multiple missions between LLO and lunar surface dedicated to crew rotation; and Multiple missions dedicated to cargo shipments within the regime of lunar surface and LLO. A complete set of structural specifications is given.
Document information
Lunar Lander Conceptual Design
1989
143 pages
Report
No indication
English
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