Base flow investigation of the Apollo AS-202 Command Module

Author:

Walpot Louis M.G.,Wright Michael J.,Noeding Peter,Schrijer Ferry

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference11 articles.

1. Lee DB, Bertin JJ, Goodrich WD. Heat transfer rate and pressure measurements obtained during Apollo Orbital entries. NASA TN D-6028; October 1970.

2. Lee DB. Apollo experience report: aerothermodynamics evaluation. NASA TN D-6843; June 1972.

3. Hillje E. Entry flight aerodynamics from Apollo Mission AS-202. NASA TN D-4185; October 1967.

4. Analysis of afterbody heating rates on the Apollo Command Modules, Part 1;Wright;Journal of Thermophysics and Heat Transfer,2006

5. Walpot L. Development and application of a hypersonic flow solver. PhD thesis. T.U. Delft University; May 2002.

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