NASA NTRS · 19760026154
Thermal boundaries analysis program document
Abstract
The digital program TBAP has been developed to provide thermal boundaries in the DD/M-relative velocity (D-V), dynamic pressure-relative velocity (q-V), and altitude-relative velocity (h-V) planes. These thermal boundaries are used to design and/or analyze shuttle orbiter entry trajectories. The TBAP has been used extensively in supporting the Flight Performance Branch of NASA in evaluating candidate trajectories for the thermal protection system design trajectory.
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Evans, M. E.. 1975-04-30. Thermal boundaries analysis program document. https://ntrs.nasa.gov/citations/19760026154
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