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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2011
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Article
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Tab 5
/
Review Article
Survey of European and Major ISC Facilities for Supporting Mars and Sample Return Mission Aerothermodynamics and Tests Required for Thermal Protection System and Dynamic Stability
Table 5
Maximum heat fluxes for EVD mission [
6
].
Trajectory
Convective flux kW/m
2
Radiative flux kW/m
2
Total flux kW/m
2
Total heat load MJ/m
2
E1
11500
7500
18800
106.9
E2
15700
18100
33800
178.3
E3
9350
4550
13900
243.2
E4
7000
1900
8900
154.6