Lightweight Thermal Protection Systems for Space Vehicle Propellant Tanks

640025

01/01/1964

Event
SAE World Congress & Exhibition
Authors Abstract
Content
Efficient storage of propellants (especially cryogenics) in space for more than a few hours will generally require the use of multiple foil insulation and/or shadow shields. The practical problems involved in applying both foil and shadow shields, and the current state-of-the-art are discussed. Performances in both an Earth and space environment are given for various foil insulated systems. Realistic weight estimates, supported by some experimental data, indicate that foil, despite its application penalties, outperforms all other nonfoil insulations; also, that shadow shield systems can be extremely lightweight and definitely should be considered for future thermal protection systems.
Meta TagsDetails
DOI
https://doi.org/10.4271/640025
Pages
16
Citation
Knoll, R., and Oglebay, J., "Lightweight Thermal Protection Systems for Space Vehicle Propellant Tanks," SAE Technical Paper 640025, 1964, https://doi.org/10.4271/640025.
Additional Details
Publisher
Published
Jan 1, 1964
Product Code
640025
Content Type
Technical Paper
Language
English