1. Overview of Heatshield for Extreme Entry Environment Technology (HEEET)
- Author
-
Driver, D. M, Ellerby, D. T, Gasch, M. J, Mahzari, M, Milos, F. S, Nishioka, O. S, Peterson, K. H, Stackpoole, M. M, Venkatapathy, E, Young, Z. W, Gage, P. J, Boghozian, T, Chavez-Garcia, J. F, Gonzales, G. L, Palmer, G. E, Prabhu, D. K, Williams, J. D, Kazemba, C. D, Murphy, A. S, Langston, S. L, Poteet, C. C, Splinter, S. C, Fowler, M. E, and Kellermann, C. M
- Subjects
Spacecraft Design, Testing And Performance - Abstract
The objective of the Heatshield for Extreme Entry Environment Technology (HEEET) projects is to mature a 3-D Woven Thermal Protection System (TPS) to Technical Readiness Level (TRL) 6 to support future NASA missions to destinations such as Venus and Saturn. Destinations that have extreme entry environments with heat fluxes > 3500 W/sq cm and pressures up to 5 atmospheres, entry environments that NASA has not flown since Pioneer-Venus and Galileo. The scope of the project is broad and can be split into roughly four areas, Manufacturing/Integration, Structural Testing and Analysis, Thermal Testing and Analysis and Documentation. Manufacturing/Integration covers from raw materials, piece part fabrication to final integration on a 1-meter base diameter 45-degree sphere cone Engineering Test Unit (ETU). A key aspect of the project was to transfer as much of the manufacturing technology to industry in preparation to support future mission infusion. The forming, infusion and machining approaches were transferred to Fiber Materials Inc. and FMI then fabricated the piece parts from which the ETU was manufactured.
- Published
- 2019