Exploration of the Viability of HEEET as a TPS for Saturn, Neptune, and Uranus EntriesExploration of ballistic coefficient and entry flight path angle to determine loom requirements for weaving a dual-layer thermal protection material such as HEEET
Document ID
20190002181
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Prabhu, Dinesh K. (Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Date Acquired
April 5, 2019
Publication Date
September 11, 2018
Subject Category
Spacecraft Design, Testing And PerformanceLunar And Planetary Science And Exploration