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Common lunar lander (cll) conceptual design and mass properties
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lawson, Shelby |
| Copyright Year | 1991 |
| Description | The conceptual design and mass properties are presented for the CLL in viewgraph format. The spacecraft structural mass is given for orbital assembly, thermal insulation, integrated propulsion, power generation, avionics, environment control, and pyrotechnics and landing system. The mass is given of the lander as well as the transfer stage. |
| File Size | 533706 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19920009591 |
| Archival Resource Key | ark:/13960/t6g20wq14 |
| Language | English |
| Publisher Date | 1991-09-17 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Pyrotechnics Structural Weight Systems Engineering Thermal Insulation Landing Aids Orbital Assembly Spacecraft Design Propulsion System Configurations Avionics Lunar Landing Environmental Control 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 |
