Approximate Pressure Distribution in an Accelerating Launch-Vehicle Fuel Tank
Author:   National Aeronautics and Space Adm Nasa
Publisher:   Independently Published
ISBN:  

9781794298095


Pages:   36
Publication Date:   19 January 2019
Format:   Paperback
Availability:   Available To Order   Availability explained
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Approximate Pressure Distribution in an Accelerating Launch-Vehicle Fuel Tank


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Overview

A detailed derivation of the equations governing the pressure in a generic liquid-fuel launch vehicle tank subjected to uniformly accelerated motion is presented. The equations obtained are then for the Space Shuttle Superlightweight Liquid-Oxygen Tank at approximately 70 seconds into flight. This generic derivation is applicable to any fuel tank in the form of a surface of revolution and should be useful in the design of future launch vehicles Nemeth, Michael P. Langley Research Center NASA/TM-2010-216681, NF1676L-10237, L-19835

Full Product Details

Author:   National Aeronautics and Space Adm Nasa
Publisher:   Independently Published
Imprint:   Independently Published
Dimensions:   Width: 21.60cm , Height: 0.20cm , Length: 27.90cm
Weight:   0.109kg
ISBN:  

9781794298095


ISBN 10:   1794298096
Pages:   36
Publication Date:   19 January 2019
Audience:   General/trade ,  General
Format:   Paperback
Publisher's Status:   Active
Availability:   Available To Order   Availability explained
We have confirmation that this item is in stock with the supplier. It will be ordered in for you and dispatched immediately.

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