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Apollo experience report: lunar module structural subsystem
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Weiss, S. P. |
| Copyright Year | 1973 |
| Description | In the Apollo Program, the lunar-orbit rendezvous mode was used for the lunar-landing mission. To accomplish the lunar landing, a lunar module spacecraft was built. A description of the design requirements for the structural subsystem and of the structural configuration and the method of design verification are given. A discussion is presented of several problems encountered and the corrective actions taken during the designing, manufacturing, and testing of the lunar module. |
| File Size | 1370004 |
| Page Count | 22 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730010174 |
| Archival Resource Key | ark:/13960/t97707x2t |
| Language | English |
| Publisher Date | 1973-03-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Equipment Specifications Systems Engineering Apollo Project Manufacturing Spacecraft Design Spacecraft Configurations Lunar Module 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 |
