File:Ablative heat shield studies for NASA Mars-Earth return entry vehicles (IA ablativeheatshie1094534895).pdf

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Ablative heat shield studies for NASA Mars/Earth return entry vehicles   (Wikidata search (Cirrus search) Wikidata query (SPARQL)  Create new Wikidata item based on this file)
Author
Hamm, Michael K.
image of artwork listed in title parameter on this page
Title
Ablative heat shield studies for NASA Mars/Earth return entry vehicles
Publisher
Monterey, California: Naval Postgraduate School
Description

A material that behaves likes a glassy ablator on the surface, has a low thermal conductivity, is structurally tough, lightweight, and is in some sense reusable, would be desirable for the protective heat shield used on Earth entry vehicles. A material for this purpose has been developed that uses silicon dioxide (fused quartz) in a fibrous packed matrix, forming blocks which can behave as a glassy ablator on the surface when subject to very high surface heat fluxes. These fibrous silicon dioxide blocks are called Reusable Surface Insulation (RSI). The primary constituent of the RSI material is silicon dioxide, but may contain other compounds (e.g. alumina borosilicate) to affect the thermal and physical properties. The research performed in this thesis is to determine the ablative behavior of ceramic RSI materials in a hypersonic high enthalpy flow that is used to simulate entry into Earth atmosphere. Actual arc jet experiments were performed to measure mass loss, melt run off, and fiber collapse of these materials and compare the experimental results with predicted theoretical values. The tests were performed to ascertain if RSI type materials could be used for entry vehicles proposed in NASA Mars missions.


Subjects: Space vehicles; Atmospheric entry; Mars (Planet); Ablative materials; Shielding (Heat); Ablative; hypersonic; NASA; Mars; heat shield
Language English
Publication date September 1990
publication_date QS:P577,+1990-09-00T00:00:00Z/10
Current location
IA Collections: navalpostgraduateschoollibrary; fedlink
Accession number
ablativeheatshie1094534895
Source
Internet Archive identifier: ablativeheatshie1094534895
https://archive.org/download/ablativeheatshie1094534895/ablativeheatshie1094534895.pdf
Permission
(Reusing this file)
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, may not be copyrighted.

Licensing[edit]

Public domain
This work is in the public domain in the United States because it is a work prepared by an officer or employee of the United States Government as part of that person’s official duties under the terms of Title 17, Chapter 1, Section 105 of the US Code. Note: This only applies to original works of the Federal Government and not to the work of any individual U.S. state, territory, commonwealth, county, municipality, or any other subdivision. This template also does not apply to postage stamp designs published by the United States Postal Service since 1978. (See § 313.6(C)(1) of Compendium of U.S. Copyright Office Practices). It also does not apply to certain US coins; see The US Mint Terms of Use.

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current06:37, 8 July 2020Thumbnail for version as of 06:37, 8 July 20201,275 × 1,650, 122 pages (2.9 MB) (talk | contribs)FEDLINK - United States Federal Collection ablativeheatshie1094534895 (User talk:Fæ/IA books#Fork8) (batch 1990-1992 #2770)

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