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Stagnation point radiative heating relations for venus entry
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Palmer, Grant E. Tauber, Michael E. Prabhu, Dinesh K. |
| Copyright Year | 2012 |
| Description | Improved analytic expressions for calculating the stagnation point radiative heating during entry into the atmosphere of Venus have been developed. These analytic expressions can be incorporated into entry trajectory simulation codes. Together with analytical expressions for convective heating at the stagnation point, the time-integrated total heat load at the stagnation point is used in determining the thickness of protective material required, and hence the mass of the fore body heatshield of uniform thickness. |
| File Size | 189168 |
| Page Count | 6 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20120001655 |
| Archival Resource Key | ark:/13960/t35190g7k |
| Language | English |
| Publisher Date | 2012-01-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Thermodynamics Thickness Venus Atmosphere Computation Aerodynamic Heating Stagnation Point Heat Shielding Radiative Transfer Planetary Landing Pioneer Venus Spacecraft Computerized Simulation Atmospheric Entry Heat Transfer Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
