1. An Analysis of the Radiative Heating Environment for Aerocapture at Titan
2. (b) 1800lines/mm, Us=6.02km/s Figure 11. NRST-Al spectral volumetric radiance and its cumulative integration for at the axial location of the nonequilibrium peak. For all conditions, the freestream pressure was 13Pa.
3. (b) 1800lines/mm, Us=6.76km/s
4. (b) 1800lines/mm, Us=5.95km/s Figure 13. NRST-Al spectral volumetric radiance and its cumulative integration for at the axial location of the nonequilibrium peak. For all conditions, the freestream pressure was 8Pa.
5. (b) 1800lines/mm, Us=9.80km/s