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System design of the pioneer venus spacecraft. volume 5: probe vehicle studies
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Nolte, L. J. Stephenson, D. S. |
| Copyright Year | 1973 |
| Description | A summary of the key issues and studies conducted for the Pioneer Venus spacecraft and the resulting probe designs are presented. The key deceleration module issues are aerodynamic configuration and heat shield material selection. The design and development of the pressure vessel module are explained. Thermal control and science integration of the pressure vessel module are explained. The deceleration module heat shield, parachute and separation/despin are reported. The Thor/Delta and Atlas/Centaur baseline descriptions are provided. |
| File Size | 301509105 |
| Page Count | 632 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740019262 |
| Archival Resource Key | ark:/13960/t1ck35m0m |
| Language | English |
| Publisher Date | 1973-07-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Pioneer Space Probes Venus Probes Aerodynamic Configurations Pressure Vessels Systems Engineering Heat Shielding Thor Delta Launch Vehicle Spacecraft Design 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 |
