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System design of the pioneer venus spacecraft. volume 4: probe bus and orbiter spacecraft vehicle studies
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Bozajian, J. M. |
| Copyright Year | 1973 |
| Description | The requirements, trades, and design descriptions for the probe bus and orbiter spacecraft configurations, structure, thermal control, and harness are defined. Designs are developed for Thor/Delta and Atlas/Centaur launch vehicles with the latter selected as the final baseline. The major issues examined in achieving the baseline design are tabulated. The importance of spin axis orientation because of the effect on science experiments and earth communications is stressed. |
| File Size | 12455814 |
| Page Count | 259 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740019261 |
| Archival Resource Key | ark:/13960/t2c872h0q |
| Language | English |
| Publisher Date | 1973-07-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Pioneer Space Probes Venus Probes Space Missions Systems Engineering Thor Delta Launch Vehicle Mission Planning Spacecraft Stability Atlas Centaur Launch Vehicle Spacecraft Configurations 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 |
