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Apollo experience report guidance and control systems: lunar module abort guidance system
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kurten, P. M. |
| Copyright Year | 1975 |
| Description | The history of a unique development program that produced an operational fixed guidance system of inertial quality is presented. Each phase of development, beginning with requirement definition and concluding with qualification and testing, is addressed, and developmental problems are emphasized. Software generation and mission operations are described, and specifications for the inertial reference unit are included, as are flight performance results. Significant program observations are noted. |
| File Size | 4274702 |
| Page Count | 73 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750018954 |
| Archival Resource Key | ark:/13960/t6741jk6h |
| Language | English |
| Publisher Date | 1975-07-01 |
| Access Restriction | Open |
| Subject Keyword | Astronautics (general) Digital Computers Apollo Project Inertial Guidance Abort Trajectories Monte Carlo Method Lunar Module Lunar Landing 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 |
