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Pressure loss tests on plain screen samples (15mm & 30mm)

Fischer, A. (2011) Pressure loss tests on plain screen samples (15mm & 30mm). Other. DLR-Interner Bericht. RYTA-CUST-TR-02-A. (Unpublished)

Full text not available from this repository.

Abstract

Propellant Management Devices in new upper stage tank technologies use as subcomponents metallic screens. These screens are used for multiple purposes, such as to filter the propellant and oxidizer for example. But there is another major task for such screens: they are able to detain gas bubbles in a liquid flow. This is important to provide a pure liquid flow of propellant and oxidizer to the spacecraft’s engine. Regarding to this, the Bubble Point becomes important. It describes the maximum pressure difference across a screen, when gas bubbles can break through. It is of importance, that in a feed line system the pressure drop across a metallic screen device never becomes higher than the Bubble Point of the used screen. Otherwise a gas-free fluid flow cannot be provided. For that reason, and for the total pressure loss in the feed line system, it is important to know the pressure loss behaviour of metallic screen elements. DLR Bremen provides in cooperation with EADS Astrium Bremen tests for screen samples of metallic screens. This document includes the test results.

Item URL in elib:https://elib.dlr.de/103021/
Document Type:Monograph (DLR-Interner Bericht, Other)
Title:Pressure loss tests on plain screen samples (15mm & 30mm)
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Fischer, A.UNSPECIFIEDUNSPECIFIED
Date:3 November 2011
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Unpublished
Keywords:Pressure loss tests, plain Screen samples, 15mm & 30mm
Institution:DLR Bremen
Department:RY-TAS
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:other
DLR - Research area:Raumfahrt
DLR - Program:R - no assignment
DLR - Research theme (Project):R - no assignment
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Transport and Propulsion System
Deposited By: Behnke, Manuela
Deposited On:24 Feb 2016 09:49
Last Modified:10 May 2016 23:44

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