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NASA NTRS · 19920024101

First Lunar Outpost crew module thermal protection design sensitivity

Abstract

A thermal protection study was conducted on the first lunar outpost (FLO) crew module. The study objectives are as follows: (1) assess effects of vehicle size on aerothermodynamic environment and thermal protection system (TPS) weight; (2) assess effects of lunar-return strategies on aerothermodynamic environment and TPS weight; and (3) assess weight penalty for common TPS design for all lunar-return strategies. All material is covered in viewgraph format.

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BibTeXRIS

Bouslog, Stan, Rochelle, Bill, Williams, Stan, Caram, Joe, Curry, Don, Derry, Steve, Ondler, Matt. 1992-01-01. First Lunar Outpost crew module thermal protection design sensitivity. https://ntrs.nasa.gov/citations/19920024101

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