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Lunar lander conceptual design: lunar base systems study task 2.2
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1988 |
| Description | This study is a first look at the problem of building a lunar lander to support a small lunar surface base. One lander, which can land 25 metric tons, one way, or take a 6 metric ton crew capsule up and down is desired. A series of trade studies are used to narrow the choices and provide some general guidelines. Given a rough baseline, the systems are then reviewed. A conceptual design is then produced. The process was only carried through one iteration. Many more iterations are needed. Assumptions and groundrules are considered. |
| File Size | 6423365 |
| Page Count | 145 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880020470 |
| Archival Resource Key | ark:/13960/t0vq7ts8j |
| Language | English |
| Publisher Date | 1988-03-30 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Structural Design Costs Propellants Lunar Landing Modules Lunar Bases Maintenance Reusable Spacecraft Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
