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.
Thermal boundaries analysis program document
1975-04-30
Report
Keine Angabe
Englisch
Thermal Boundaries Analysis Program Document
NTIS | 1975
|Software Document Inventory Program
NTRS | 1984
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Trans Tech Publications | 2014
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